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Three isolated full-scale shear walls of low-strength autoclaved aerated concrete (AAC) were tested at the Structural Engineering Ferguson Laboratory of the University of Texas at Austin. One specimen was constructed with vertical panels, and the other two, with partially grouted reinforced masonry units. The main objective of this study is to validate previously proposed design provisions for low-strength AAC material. The variables considered in these shear wall specimens were the compressive strength of the material, the flexural reinforcement, and the geometry. Test results indicate good agreement between observed and predicted bahavior, and validate the previously proposed design provisions. The results support the extension of those design provisions to low-strength AAC shear-wall structures located in seismic zones.
This thesis is orgainzed as follows: Chapter 2 presents the characteristics of the three AAC shear wall specimens, mechanical properties of the AAC material, instrumentation and planning prior to the tests. Chapter 3 contains information obtained during the tests, including the principal observations and basic behavior of the specimens. Chapter 4 presents an evaluation of the significance of results ovtained from the tests. Finally, Chapter 5 provides the summary, conclsuions and recommendations resulting from the study.
Two Appendices are also included:
Appendix A presents the relevant theory, including the design provisions for reinforced AAC shear walls developed by Tanner and Varela.
Appendix B presents the first chapters of the current draft of the ACI 523.5 R--xx Guide for Using Autoclaved Aerated Concrete Panels. The purpose of this appendix is to present basic information on AAC, that was not developed by the author.
Test Specimens, Test Setups, and Testing Procedures
The testing program included one flexure-dominated specimen and two shear-dominated specimens, tested using the same setup and instrumentation used in previous tests by Varela and Tanner. The setup permitted the application of constant gravity loads and quasi-static, reversed cyclic in-plane shear loads to single-story AAC shear walls. The instrumentation permitted the capture of global behavior (such as displacements and loads), and local behavior (such as stresses in flexural reinforcement).
The results of the AAC material strengths are also presented. The specimens were designed using those strengths, and the wall geometry, reinforcement and axial load were chosen according to the desired mode of behavior.
In this chapter, the objectives, test setup, instrumentation, material strengths, design of specimens, loading protocol and construction of the specimens are presesnted.
2.2 DESIGN AND CONSTRUCTION OF SHEAR WALL SPECIMEN 17
Shear Wall Specimen 17 was tested to verify the previouly proposed design provisions for the case of a flexure-dominated specimen of low-strength AAC, and also to evaluate possible improvements in the performance of the wall through the incorporation of stainless-steel spiral ties between the U-blocks and the remainder of the wall. This specimen was intended to fail in flexure.With this intent, the aspect ratio, the axial load and the reinforcement of the specimen were selected.
2.2.2 Configuration of Shear Wall Specimen
The wall measured 112 in. long by 144 in. high by 8 in. thick. The height from the bottom of the wall to the line of the load application was 154 in. (3.91m). The aspect ratio of the wall (height divided by plan length) was 1.34. Figure 2.1 shows the geometry and reinforcement of Shear Wall Specimen 17.
2.2.3 Test Setup for Shear Wall Specimen 17
126.96.36.199 Base Beam
The base beam measured 304.5 in. 97.73m) long by 64 in. (1.63m) wide by 16.5 in. (0.42 m) high. To prevent sliding or uplifting, the base beam was tied to the reaction floor of the lavoratory through post-tensioned rods. Details of the base beam used for Shear Wall Specimen 17 are shown in Figure2.3.
188.8.131.52 Axial Load System
The constant axial load of 25 kips (111.2kN) was applied to the specimen by a loading beam with a weight of 5 kips (22.24 kN), and by hydraulic actuators controlled by a load maintainer that provided 20 kips (89 kN). The axial load from the load maintainer was transmitted through two threaded rods, one at each side of the specimen, and located at the center of the wall. These threaded rods were connected at the top with a steel swivel beam and to the bottom with a swivel steel box which was tied to the base beam with post-tensioned rods. Figure 2.4 shows the axial load system for Shear Wall Specimen 17.
184.108.40.206 Lateral Bracing System
The lateral bracing system, necessary to provide out-of-plane stability to the specimen, consisted of four steel cables connected to the loading beam of the specimen at four different points. Two of these cables were attached to the reaction wall, and the other two were attached to steel columns.
Horizontal load was applied to the specimen with a 60 kip hydraulic actuator, controlled by an air-operated pump. The actuator has a maximum extension of 18 in. (0.46m). Figure 2.6 shows the actuator ocnnected to the loading beam of Shear Wall Specimen 17.
220.127.116.11 Instrumentation and Data Acquisition
The global and local behavior of the specimen was verified through specific instruments to measure pressure, force and displacement. The types of instruments used include: presure transducers, load cells, force washers, linear potentiometers, and string potentiometers. Table 2.1 describes the instrumentation used in Shear Wall Specimen 17. Figure 2.7 and Figure 2.8 show the location of those instruments on the specimen.
Additionally, three strain gauges were attached to each flexural reinforcing bar at three different levels within the bottom 8 in. (200 mm). These strain gauges measured the stress induced in the flexural reinforcement during the application of the horizontal force.
18.104.22.168.2 Data Acquistion
The instruments were connected to a full-bridge, and the strain gauges, to a quarter-bridge box. The full-bridge box was excited with 10 volts and the quarter-bridge box with 2 volts, both were provided by a percision power supply. These bridge boxes were connected to a HP3852Ascanner. Analog-to-digital conversion was carried out by a National Instruments card in a Window-based microcomputer running MS Excel 7.0.
2.2.4 Loading Protocol
The lateral loading program consisted of reversed cycles to a monotonically increasing maximum load or displacement. Prior to starting the tests, an initial cycle of low-lateral load, mormally 5 kips, was applied to every specimen to check the complete setup (loading equipment, lateral bracing, instruments and data acquisition.) Initial loading cycles were applied under load control to load levels predicted to produce major events in the shear-wall specimens tested. Subsequent loading cycles were applied under displacement control. For Shear Wall Specimen 17, the loading history was switched from load to displacement control after yield of flexural reinforcement.
2.2.5 Material Strengths
22.214.171.124 Compressive Strength
Shear Wall Specimen 17 was consrtucted using AAC material corresponding to Class PAAC4, which has a specified compressive strength of 4 MPa. The compressive strength of the AAC material in that specimen was tested for compliance with that specified strength.
126.96.36.199.1 Compressive Strength
Shear Wall Specimen 17 was constructed using AAC material corresponding to Class PAAC4, which has a specified compressive strength of 4 MPa. The compressive strength of the AAC material in that specimen was tested for compliance with that specified strength.
188.8.131.52.1 Specimen Preparation and Testing Procedure for Compression Tests on AAC Cubes
Cubes for the compressive tests were prepared from the AAC material used to construct Shear Wall Specimen 17. This material had been shipped to UT from Babb International, Inc. (Adel, GA). In this thesis, it is designated "Babb 4."
Nine cubes were prepared at the Babb plant for testing according to ASTM C1386. The cubes were removed from AAC blocks using a dry circular saw to extract roughly cubical blocks of AAC. These blocks were then cut into 4 in. 9100 mm) cubes using a water-cooled circular saw. All cubes were oriented so that they would be tested perpendicular to the direction of rise.
All faces of the AAC cubes were milled using a machine with two grinding wheels that allowed milling two parappel faces of the cubes at the same time.
After the cubes were milled, their moisture content was measure by weighing. Because that moisture content exceeded the maximum value specified in ASTM C1386, the cube specimens were placed in an oven for 24 hours at a constant temperature of 140 degrees Fahrenheit. After that time, the cubes were again weighed. The weights of AAC cubes measured at Babb Plant and at UT Austin are presented in Table 2.2.
These cubes were tested at the Babb plant laboratory, and the rest were sent to UT Austion for confirmatory compressive strength tests (Varela 2003). Compression testing was performed in a universal machine, which includes a load cell and a spherical seat to apply uniform load. Data were recorded using data-acquistion software of the Ferguson Structural Engineering Laboratory of UT Austin. Figure 2.11 shows the test setup used in the compressive tests.
184.108.40.206.2 Compression Test Results for AAC Cubes
Compressive-strength results for the six specimens tested at UT Austin, summarized in Table 2.3, ranged from 737 psi (5.08 MPa) to 944 psi(6.51 MPa), with a final average of 811 psi (5.59 MPa), and a COV of 9.33%. Compressive-strength results for the three specimens tested at the Babb plant laboratory are summarized in Table 2.4. The moisture content of the cubes complied with the range of 5% to 15% specified by ASTM C1386.
2.2.6 Construction of Shear Wall Specimen 17
The surface of the base beam was roughened and pre-wetted. A leveling bed was applied, using conventional Portland cement-lime masonry mortar conforming to ASTM C270, Type S by proportion. The vertical panels were set up and joined with thin-bed mortar, and were clamped together to apply pressure to the face of the ioints. The plumbness of the panels was checked frequently during construction. The U-blocks were placed at each end of the wall, and were joined to the vertical panels using thin-bed mortar and stainless-steel spiral ties. The cores created by these U-blocks and the vertical panels were filled with coarse grout conforming to ASTM C476 by proportion and consolidated by vibrator. Figure 2.12 shows a partial view of Shear Wall Specimen 17 after construction.
2.3 DESIGN AND CONSTRUCTION OF SHER WALL SPECIMENS 18 AND 19
Shear Wall Specimens 18 and 19 were tested to verify the previously proposed design provisions for the case of a shear-dominated specimen of low-strength AAC, and also to examine the overall hysteretic behavior of the walls. These specimens were intended to fail in web-shear cracking. With this intent, their aspect ratio, axial load and flexural reinforcement were selected.
2.3.2 Configurations of Shear Wall Specimen 18 and 19
Shear Wall Specimen 18 was constructed with AAC masonry units placed in running bond. The wall measured 144 in. (3.66 m) long by 144 in. (3.66 m) high by 8 in. (0.203 m) thick. The height from the bottom of the wall to the line of the load application was 154 in. (3.91 m). The aspect ratio of the wall (height divided by plan length) was 1.07. The threaded rods used as external flexural reinforcement corresponded to ASTM A193-B7 bars 1 in. (25.4 mm) in diameter. Figure 2.13 shows the geometry and reinforcement of Shear Wall Specimen 18.
Shear Wall Specimen 19 was constructed with AAC masonry units placed in running bond. The wall measured 216 in. (5.49 m) long by 144 in. (3.66 m0 high by 8 in. (0.203 m) thick. The height from the bottom of the wall to the line of the load application was 154 in. (3.91 m). The aspect ratio of the wall (height divided by plan length) was 0.71. The threaded rods used as external flexural reinforcement corresponded to ASTM A193-B7 bars 1 in. (25.4 mm) in diameter. Fugure 2.14 shows the geometry and reinforcement of Shear Wall Spceimen 19.
2.3.3 Test Setup for Shear Wall Specimens 18 and 19
220.127.116.11 Base Beam
The foundation used for Shear Wall Specimens 18 and 19 was a base beam with identical geometric characteristics to that of the base used for Shear Wall Specimen 17.
18.104.22.168 Axial Load System
An axial load of 45 kips (200.12 kN) was applied to Shear Wall Specimen 18 by a loading beam with a weight of 5 kips (22.24 kN) and four threaded rods post-tensioned manually which provided 40 kips (177.88 kN) in total. These threaded rods, two at each end of the specimen, were connected at the top with transverse steel beams and to the bottom with steel boxes which were tied to the base beam with bolts (post-tensioned rods). Figure 2.16 shows the axial load system used for Shear Wall Specimen 18.
An axial load of 58 kips(258 kN) was applied to Shear Wall Specimen 19 by a loading beam with a weight of 8 kips (35.58) and four threaded rods post-tensioned manually to provide 50 kips (222.4 kN) in total. The setup of these threaded rods was the same as for Shear Wall Specimen 18. Figure 2.17 shows the axial load system used for Shear Wall Specimen 19.
22.214.171.124 Lateral Bracing System
The lateral bracing system was necessary to provide out-of-plane stability to the specimens. The system was identical to that used for Shear Wall Specimen 17.
The actuator was identical to that used for Shear Wall Specimen 17.
126.96.36.199 Instrumentation and Data Acquistion
The global and local behavior of both specimens was verified through specific instruments to measure pressure, force and displacement. The types of instruments used include: preesure transducers, load cells, force washers, linear potentionmeters, and string potentiometers. Table 2.5 describes the instrumentation sued in Shear Wall Specimens 18 and 19. Figure 2.18 and Figure 2.19 show the location of that instrumentation in Shear Wall Specimen 18. The same configuration of instrumentation was used in Shear Wall Specimen 19.
Additionally, two strain gauges were attached to each extreme flexural reinforcing bar at two different levels within the bottom 4 in. (100 mm). These strain gauges measured the stress induced in the flexural reinforcement during the application of the horizontal force. The strain-gauge positions in Shear Wall Specimens 18 and 19 were similar to those used in Shear Wall Specimen 17.
188.8.131.52.2 Data Acquistion
The data acquisition system and connection of the instrumentation used in Shear Wall Specimens 18 and 19 were the same as those used for Shear Wall Specimen 17.
2.3.4 Loading Protocol
The lateral loading program used for Shear Wall Specimens 18 and 19 was similar to that used for Shear Wall Specimen 17. For the shear-dominated specimens, the loading history was switched from load to displacement control after web-shear cracking.
2.3.5 Material Strengths
184.108.40.206 Compressive Strength
Shear Wall Specimens 18 and 19 were constructed using AAC material corresponding to Class PAAC2, which has a specified compressive strength of 2 MPa (290 psi). The compressive strength of the AAC material in those specimens was tested for compliance with that specified strength, using cubes prepared at the Babb plant and cores taken from masonry type units at UT Austin.
220.127.116.11.1 Specimen Preparation and Testing Procudure for Compression Tests on AAC Cores
Cores for the compressive tests were prepared from the AAC material used to construct Shear Wall Specimen 18 and 19. This material had been shipped to UT from Babb International, Inc. (Adel, GA). In this thesis, that maerial is designated "Babb 3."
Nine cores were prepared at UT for testing according to the same protocol prescribed for testing cubes in ASTM C1386. The cores were removed from the center and the outer third of AAC units, and measured 7 13/16 in. (198 mm) long by 3 11/16 in. (94 mm) in diameter. Their aspect ratio (length divided by diameter) was 2.
After the cores were extracted, their weight, density and moisture contents were measured. The moisture content of the cores must be between 5 % and 15% according to ASTM C1386. The moisture content (MC) was measured three times: at the time of the compressive test; at the end of the test; and five days after the end of the test as a confirmation of the dry density. Table 2.6 shows the moisture content recorded from the cores.
The compressive test setup included an extensometer attached to a linear potentiometer with a 2-inch range of measuring the axial deformation during the test. Thes test was performed in a universal testing machine, which includes a load cell and a spherical head to apply uniform load to cores. Data were recorded using data-acquisition software of the Ferguson Structural Engineering Laboratory of UT Austin. Figure 2.20 shows the test setup used in the compressive tests.
18.104.22.168 Compression Test Results for AAC Cores
Compressive strengths for the six cores, summarized in Table 2.7, ranged from 287 psi (1.99 MPa) to 370 psi (2.57 MPa), with a mean of 344 psi (2.39MPa) and a COV of 8.13%. Figure 2.21 shows the stress-strain curves ovtained for the six cores.
The range of maximum strains was less than 0.003, and was also less than the values reported by Tanner (2003). To investigate this apparent discrepancy, the maximum strain values of this study and those of previous studies were investigated further, and are discussed immediately below.
22.214.171.124 Further Comments on Maximum Useful Strain
Table 2.8 summarizes for each lot of material, the mean maximum useful strain reported in this study and the values reported by Tanner (2003). Figure 2.22 is a graph of those maximum strain values as a function of tested compressive strength.
Figure 2.22 shows a clear tendency for the maximum useful strain of AAC to decrease with decreasing compressive strength. Results reported in this thesis for low-strength AAC are consistent with those reported proviously by Tanner (2003).
In provious work by Tanner (2003), Varela (2003) and Argudo (2003), the value of was reported as a constant 0.003, independent of compressive strength. Though not used directly in design provisions, is indirectly related to vital behavioral characteristics such as nominal flexural capacity, and the available ductility and drift capacities used to establish appropriate values of R and C.
Because is apparently lower for low-strength AAC, the behavior of structural elements of low-strength AAC must be carefully reviewed to ensure that previously devepoled expressions for nominal flexural capacity and ductility and drift capacity are applicable to low-strength AAC as well. Paraenthetically, one would expect the nominal flexural capacity of AAC elements to be governed by mechanical characteristics of the reinforcement in all practical cases, and therefore not snsitive to. One would also expect ductility and drift capacity to be directly verifiable from wall tests. In subsequent chapters of this thesis, those comparisons are made.
It is also necessary to examine the internal consistency of stress-strain data reported here for low-strength AAC, with that reported by Tanner (2003). That comparison is presented in Table 2.9, in terms of tested versus specified compressive strengths and observed versus predicted values of AAC. In that table, the relationship between observed and specified compressive strength for low-strength AAC is seen to be consistent with those for higher-strength AAC. Additionally, the relationship between observed AAC and that prdicted by Equation 2.1 is seen to be consistent with that reported previously for higher-strength AAC.
2.3.6 Splitting Tensile Strength
Shear Wall Specimens 18 and 19 were constructed using AAC material corresponding to Class PAAC2, which has a specified compressive strength of 2 MPa (290 psi). The tensile strength of the AAC material in those specimens was tested.
126.96.36.199 Specimen Preparation and Testing Procudure for Splitting Tensile Tests on AAC masonry Units
Unites for the splitting tensile tests were prepared from the AAC material used to construct Shear Wall Specimens 18 and 19. This material had been shipped to UT from Babb International, Inc. (Adel, GA). In this thesis, it is designated as "Babb 3."
Six Units were prepared at UT for testing according to ASTM C1006. The measurements of these units were 7 13/16 in. 9198 mm0 high by 7 13/16 in. (198 mm) wide by 24 in. (610 mm) long.
After the units were prepared, their weight, density and moisture contents were measured. The moisture content of the units must be between 5% and 15% according to ASTM C1386. The moisture content 9MC) was measured three times; at the time of the tensile test, at the end of the test, and five days after the end of the test. Table 2.10 shows the moisture content recorded from the units.
The test was performed in a universal machine, where the masonry units were placed between two rods, one at the bottom face and the other at the tope face. Data were recorded using the readings of the universal machine. Figure 2.23 shows the test setup used in the splitting tensile tests.
188.8.131.52 Splitting Tensile Strength for AAC Units
Splitting tensile strength for the six units, summarized in Table 2.11, ranged from 49.02 psi (0.34 MPa) to 58.41 psi (0.40 MPa), with a mean of 52.85 psi (0.37 MPa) and a COV of 6.99%.
The results obtained for the tensile strength ranged from 16% and 21% of the specified compressive strength of 290 psi (2 MPa), and from 14% to 17% of the mean tested compressive strength of 344 psi (2.37 MPa).
184.108.40.206 Comparison between observed and predicted splitting tensile strength of AAC
Through tensile strength tests performed at the University of Texas at Austin and elsewhere, an equation (Equation 2.2) to predict the tensile strength of AAC has been proposed (Argudo 2003).
The predicted tensile strength obtained using a specified compressive strength of 290 psi (2 MPa) into Equation 2.2 was40.87 psi(0.28 MPa). This value corresponds to the 77% of the average tensile value ovtained from the tests which represents a conservative estimation of the real value. On the other hand, after the evaluation of Equation 2.2 with the average compressive strength of 344 psi (2.37 MPa) obtained from the test a tensile strength of 44.51 psi (0.31 MPa) was obtained which corresponds to 84.22%, of the average tensile value. Figure 2.24 shows this last result (UT). Clearly, the relation between splitting tensile strength and tested compressive strength for low-strength AAC, is consistent with that obtained previously for higher-strength AAC.
2.3.7 Construction of Shear Wall Specimens 18 and 19
The surface of the base beam was roughened and pre-wetted. A leveling bed was applied, using conventional Portland cement-lime masonry mortar conforming to ASTM C270, Type S by proportion. The masonry units were set up in running bond and joined with tin-bed mortar. To prevent horizontal misalignment, a guide string was connected to two guide poles located at each end of the walls. The plumb was also checked every three courses during the construction. Figure 2.25 shows construction details of Shear Wall Specimen 19.
Figure 2.26 and Figure 2.27 show views of Shear Wall Specimens 18 and 19 respectively, after construction.
Test Results for AAC Shear Wall Specimens
The objective of this chapter is to describe the results obtained from the flexure-dominated wall (SWS 17) and the shear-dominated walls (SWS18 and SWS19). The results ovtained for each specimen are accompanied by the objectives, loading history, description of the major events observed during the testm and hysteretic behavior of the walls. Design of each shear wall specimen comprised the folloing steps: selection of plan length, which, in combination with a constant specimen height, defined the specimen's aspect ratio; selection of the amount and distribution of flexural reinforcement, to encourage the desired behavior; prediction of each liimit state, based on that aspect ratio and flexural reinforcement, using interation diagrams of base shear capacity as a function of axial load; and iteration of aspect ratio, flexural reinforcement and axial load to produce a specimen with the intended behavior. When each specimen was tested, its observed capacity in relevant limit states was compared with the corresponding predicted capacity.
3.2 TEST RESULTS FOR SHEAR WALL SPECIMEN 17
The behavior of Shear Wall Specimen 17 is predicted using the interaction diagram of Figure 3.1. In that interaction diagram, relevant behavior modes of the specimen are represented, including flexural cracking, flexure-shear cracking, sliding shear, web-shear cracking, and nominal flexural capacity. The applied axial load for Shear Wall Specimen 17 was selected as 25 kips (111.2 kN). At this axial load, the major events in order of occurrence were flexural cracking, flexure-shear cracking, and nominal flexural capacity. Web-shear cracking, sliding shear, and crushing of the diagonal strut are not expected to occur because the curves coorresponding to them lie to the right of curve represenging nominal flexural capacity.
3.2.1 Loading History and Major Events for Shear Wall Specimen 17
The actual loading and displacement histories for Shear Wall Specimen 17 are presented in Figure 3.2 and Figure 3.3 respectively. The numbers on the graphs refer to load points (each point during the test when data were reocrded). Positive values of the base shear force correspond to loading to the south, and negative values, to loading to the north. Each cycle is subdiveded into an "a" protion (positive displacements) followed by a "b" portion (negative displacements). For each cycle of loading, the maximum loads and drift ratio are shown in Table 3.1.
3.2.2 Sequence of Crack Formation for Shear Wall Specimen 17
The behavior of Shear Wall Specimen 17 is described through major events observed during the test. These major events refer to significant changes in the condition of the specimen. In Table 3.2, each major event is matched with its respecive load point and the corresponding changes in the specimen. In the remainder of this section, each major event is discussed further.
220.127.116.11 Flextral Cracking in Shear Wall Specimen 17
According to Table 3.2, Major Events 1 and 2 correspond to flexural cracking at the north end and the south ends of the specimen respectively. At the north end of the specimen (loading to the south0, flexural cracking occurred at a load of 11.41 kips (50.8 kN) and a drift ratio of 0.026% (Load Point 176). At the south end of the specimen (loading to the north) flexural cracking occurred at a load of 18.81 kips (83.72 kN) and a drift ratio of 0.053% (Load Point 348). Flexural cracking was predicted at a base shear of 12.1 kips (53.82 kN). The ratios of observed to prdicted cracking strength were 0.94 (loading to the south) and 1.55 (loading to the north).
As the test progressed, these flexural cracks propagated toward the center of the specimen from both ends. These observations correspond to Major Events 3 and 4, which were recorded at Load Point 306 (loading to the south) and Load Point 351 (loading to the north). This cracking pattern is shown in Figure 3.4.
18.104.22.168 Flexure-shear cracking in Shear Wall Specimen 17
Major Events 5 and 6 denote the formation of flexure-shear cracks while loading south and north respectively. At the north end (loading to the south), these cracks formed at a base shear of 25.31 kips (112.63 kN) and a drift ratio of 0.13% (Load Point 508). This flexure-shear crack formed at the first and second U-blocks at the bottom of Shear Wall Specimen 17, and continues to the middle of the first panel at the north end of the specimen. These cracks are shown in detail in Figure 3.5.
At the south end (loading to the north), these cracks formed at a base shear of 24.34 kips (108.6 kN) and a drift ratio of 0.082% (Load Point 547). Flexural-shear cracking was predicted at a base shear of 23.09 kips (102.7 kN). The ratios of observed to predicted flexure-shear cracking strength were 1.09 (loading to the south) and 1.05 (loading to the north).
Yielding of the flexural reinforcement was observed at a base shear of 25.0 kips (111.2 kN) (loading to the south). This observation corresponds to Major Event 7.
As the test progressed, existing flexure-shear cracks propagated at both ends of the specimen.
Yielding of the flexural reinforcement was observed at a base shear of 25.0 kips (111.2kN) (loading to the south). This observation corresponds to Major Event 7.
As the test progressed, existing flexure-shear cracks propagated at both ends of the specimen. Additional flexure-shear cracks propagated at both ends of the specimen. Additional flexure-shear cracks formed at approximately 12 in. (0.30m) and 24 in. (0.61 m)
from the bottom of the wall as the applied load increased to 26.03 kips (115.83 kN) loading to the south, and to 27.86 kips (123.97 kN) loading to the north. These observations also correspond to Major Event 7 (Load Point 600) and Major Event 8 (Load Point 645). This cracking pattern is shown in Figure 3.6.
22.214.171.124 Additional Cracking in Shear Wall Specimen 17
Major Events 9 and 10 correspond to the formation of additional flexure-shear cracks and the development of vertical cracks in Shear Wall Specimen 17. At the north end, additional flexure-shear cracks formed at Load Point 845, which corresponded to a base shear of 32.11 kips (142.89 kN). These cracks were located approximately 5 ft. (1.52m) from the base of the specimen, and propagated from its north extreme fiber to the middle of the first panel. At Load Point 935, similar crack propagation occurred at the south end, at a base shear of 33.28 kips (148.12 kN). Vertical cracks formed between the first and second vertical panels at the north end of the specimen and between the fourth vertical panel and the U-block at the south end of the specimen, approximately 6 ft. (1.83m) from the bottom of the wall.
Major Events 11 and 12 correspond to propagation of previously formed flexure-shear cracks. These observations correspond to Load Point 940 and Load Point 978, loading to the north and south respectively. Figure 3.7 shows the pattern of cracks at this stage of the test.
126.96.36.199 Final damage in Shear Wall Specimen 17
The final stage of testing of Shear Wall Specimen 17 was Major Event 13, which denoted progressive damage at both ends of the specimen, as the previously formed flexure-shear cracks propagated toward the center and the mid-height of the wall. At Load Point 1121, which corresponded to a base shear of 17.81 kips (79.25 kN), toe spalling and crushing started at the north end. This damage, along with yield of the flexural reinforcement, resulted in a gradual and continuous drop in the in-plane lateral stiffness of the specimen. Capacity was limited by fracture of flrxural reinforcement at the north end of the specimen(while loading to the south), and was later confirmed as brittle fracture by the absence of necking of the affected bar.
Figure 3.8 shows the damage in Shear Wall Specimen 17 at the end of the test. The significant spalling at the bottom of the north end of the specimen during the final increments of load is shown in Figure 3.9 and Figure 3.10.
3.2.3 Load-Displacement Behavior of Shear Wall Specimen 17
The overall hysteretic behavior of Shear Wall Specimen 17 is shown in Figure 3.11. The initial stiffness of the load-displacement curve was 111 kip/in. (16 kN/mm). Flexural reinforcement yielded at a base shear of 25 kips (111.2 kN) and a corresponding displacement of 0.18 in. (0.45 mm). The test was stopped at a tip displacement of 1 in. (25 mm) because the flexural reinforcement fractured at the north end of the specimen.
3.3 TEST RESULTS FOR SHEAR WALL SPECIMEN 18
The behavior of Shear Wall Specimen 18 is predicted using the interaction diagram of Figure 3.12. In that interaction diagram, relevant behavior modes of the specimen are represented, including flexural cracking, sliding shear, web-shear cracking, crushing of the diagonal strut and nominal flexural capacity. The applied axial load for Shear Wall Specimen 18 was selected as 45 kips(200.5 kN). At this axial load, the major events in order of occurrence were flexural cracking, web-shear cracking, crushing of diagonal strut, sliding shear failure, flexure-shear cracking and yielding of flexural reinfrocement. Sliding shear cracking, flexure-shear cracking and yielding of flexural reinforcement were not expected to occur, because the curves corresponding to them lie to the right of the curve representing web-shear cracking failure.
3.3.1 Loading History and Major Events for Shear Wall Specimen 18 are presented in Figure 3.13 and Figure 3.14 respectively. The numbers on the graphs refer to load points (each point during the test when data were recorded). Positive values of the base shear force correspond to loading to the south, and negative values, to loading to the north. Each cycle is subdivided into an "a" protion (positive displacements) followed by a "b" portion (negative displacements). The procedure of loading the specimen was started by loading toward the south. For each cycle of loading, the maximum loads and drift ratios are shown in Table 3.3
3.3.2 Sequence of Crack Formation for Shear Wall Specimen 18
The behavior of Shear Wall Specimen 118 is described through major events observed during the test. These major events refer to significant changes in the condition of the specimen. Each major event is matched with its respective load point and the corresponding changes in the specimen, in Table 3.4. In the remainder of this section, each major event is discussed further.
188.8.131.52 Flexural cracking in Shear Wall 18
According to Table 3.4, Major Events 1 and 2 correspond to flexural cracking at the north and south ends of the specimen respectively. At the north end of the specimen (loading to the south), flexural cracking occurred at a load of 22.63 kips (100.69 kN) and a drift ratio of 0.068% (Load Point 441). At the south end of the specimen (loading to the north) flexural cracking occurred at a load of 24.99 kips (111.23 kN) and a drift ratio of 0.062 % (Load Point 509). Flexural cracking was predicted at a base shear of 19.0 kips (84.51 kN). The ratios of observed to predicted cracking strength were 1.19 (loading to the south) and 1.32 (loading to the north).
As the test progressed, these flexural cracks propagated toward the center of the specimen from both ends. These observations correspond to Major Events 3 and 4, which were recorded at Load Point 456 (loading to the south) and Load Point 517 (loading to the north). This cracking pattern is shown in Figure 3.15.
184.108.40.206 Web-shear cracking in Shear Wall Specimen 18
Major Events 5 and 6 denote the formation of web-shear cracking while loading south and north respectively. At the north end (loading to the south), these cracks formed at a base shear of 36.07 kips (160.5 kN) and a drift ratio of 0.16% (Load Point 689). This web-shear crack formed at the third and fifth course of blocks approximately 24 in. (0.61m) and 40 in. (1.02 m) from the bottom of Shear Wall Specimen 18. These cracks are shown in detail in Figure 3.16.
At the south end (loading to the north0, these cracks formed at a base shear of 35.66 kips (158.70 kN) and a drift ratio of 0.120% (Load Point 754). Web-shear cracking was predicted at a base shear of 37.0 kips (164.58 kN). The ratios of observed to predicted web-shear cracking strength were 0.97 (loading to the south) and 0.96 (loading to the north).
As the test progressed, existing web-shear cracks propagated at both ends of the specimen. Additional web-shear cracks formed in the fifth course of units, approximately 40 in. (1.02 m) from the bottom of the wall as the applied load increased to 38.59 kips (171.71 kN), loading to the south and 38.63 kips (171.92 kN), loading to the north. These observations correspond to Major Event 7 (Load Point 696) and Major Event 8 (Load Point 763). The corresponding cracking pattern is shown in Figure 3.17.
220.127.116.11. Propagation and Additional Web0shear cracking in Shear Wall Specimen 18
Major Events 9 and 10 correspond to the prpagation of existing web-shear cracks and the development of new web-shear cracks in Shear Wall Specimen 18. At the north end, additional web-shear cracks formed at Load Point 952 which corresponded to a base shear force of 40.69 kips (181.07 kN). These cracks were located along the height of the wall and spread from the north end of the specimen showed a major level of damage, with a large amount of cracking developing toward the center of the wall. This cracking pattern showed that the specimen was close to toe crushing. The cracking pattern associated with Major Events 9 and 10 is shown in Figure 3.18.
18.104.22.168 Final damage in Shear Wall Specimen 18
Major Events 11 and 12 denotes the final stage in the test of Shear Wall Specimen 18, adn were associated with progressive damage at both ends of the specimen. This damage consisted of the propagation and formation of additional web-shear cracks extended through the units and the mortar joints. At Load Point 1034, corresponding to a base shear of 35.03 kips (155.87 kN), toe crushing was observed at the south end of the specimen. An analogous situation occurred at the north end at Load Point 1089, which corresponded to a base shear of 34.73 kips (154.54 kN). At this stage, the specimen showed toe crushing at both ends, and significant reductions in in-plane stiffness (about 21% of the initial stiffness) and shear capacity. This observation is base on the reduction in slope showed by the hysteretic curve. The test was ended in Loading Cycle 10, at a maximum base shear of 31.82 kips (141.59 kN).
Figure 3.19 shows the damage in Shear Wall Specimen 18 at the end of the test. The significant extent and width of web-shear cracks are shown in Figure 3.20 and Figure 3.21.
3.3.3 Load-Displacement Behavior for Shear Wall Specimen 18
The overall hysteretic behavior of Shear Wall Specimen 18 is shown in Figure 3.22. The maximum drift ratio for this specimen was about 0.48% in both directions. The test was stopped at in-plane displacements of 0.73 in. (18.54 mm).
3.4 SHEAR WALL SPECIMEN 19
The behavior of Shear Wall Specimen 19 was predicted using the interaction diagram of Figure 3.23. In that interaction diagram, relevant behavior modes of the specimen are represented, including flexural cracking, sliding shear, web-shear cracking, crushing of the diagonal strut and nominal flexural capacity. The applied axial load for Shear Wall Specimen 19 was selected as 58 kips (258.0 kN). At this axial load, the major events in order of occurrence were flexural cracking, web-shear cracking, crushing of diagonal strut, sliding shear failure, and yielding of flexural reinforcement. Sliding shear cracking and yielding of flexural reinforcement are not expected to occur because the curves corresponding to them lie to the right of the curve representing web-shear cracking failure.
3.4.1 Loading History and Major Events for Shear Wall Specimen 19
The actual loading and displacement histories for Shear Wall Specimen 19 are presented in Figure 3.24 and Figure 3.25 respectively. The numbers on the graphs refer to load points (each point during the test when data were recorded). Positive values of the base shear force correspond to loading to the south, and negative values, to loading to the north. Each cycle is subdivided into an "a" portion (positive displacements) followed by a "b" portion (negative displacements). The procedure of loading the specimen was started by loading toward the south. For each cycle of loading, the maximum loads and drift ratios are shown in Table 3.5.
3.4.2 Sequence of Crack Formation for Shear Wall Specimen 19
The behavior of Shear Wall Specimen 19 is described through major events observed during the test. These major events refer to significant changes in the condition of the specimen. Each major event is mateched with ites respective load point and the corresponding changes in the specimen, in Table 3.6. In the remainder of this section, each major event is discussed further.
22.214.171.124 Flexural cracking in Shear Wall Specimen 19
According to Table 3.6, Major Events 1 and 2 correspond to flexural cracking at the north end and the south end of the specimen respectively. At the north end of the specimen (loading to the south), flexural cracking occurred at a load of 39.06 kips (173.82 kN) and a drift ratio of 0.062 % (Load Point 304). At the south end of the specimen (loading to the north) flexural cracking occurred at a load of 25.07 kips (111.58 KN) and a drift ratio of 0.028% 9Load Point 357). Flexural cracking was predicted at a base shear of 43.0 kips (191.26 kN). The ratio of observed to predicted cracking strength were 0.91 (loading to the south) and 0.58 9loading to the north).
As the test progressed, these flexural cracks propagated toward the center of the specimen from both ends. These observations correspond to Major Events 3 and 4, which were recorded at Load Point 317 9loading to the south) and Load Point 376 (loading to the north).This cracking pattern is shown in Figure 3.26.
126.96.36.199 Web-shear cracking in Shear Wall Specimen 19
Major Events 5 and 6 denote the formation of web-shear cracking while loading south and north respectively. At the north end (loading to the south), these cracks formed at a base shear of 56.00 kips (249.21 kN) and a drift ratio of 0.126% (Load Point 751). This web-shear crack formed approximately in the central
portion of the specimen and covered Shear Wall Specimen 19 from top to bottom. These cracks are shown in detail in Figure 3.27.
At the south end (loading to the north), these cracks formed at a base shear force of 54.84 kips (244.04 kN) and a drift ratio of 0.086% (Load Point 828). Web-shear cracking was predicted at a base shear of 52.0 kips (231.30 kN). The ratios of observed to predicted web-shear cracking strength were 1.07 (loading to the south) and 1.05 (loading to the north).
As the test progressed, flexure-shear cracking was observed at Load Point 884, which corresponded to Major Event 7. This cracking was located at the north end of the specimen, approximately 30 in. (0.76 m) from the bottom of Shear Wall Specimen 19. Major Event 8, which corresponded to Load Point 890 and a base shear force of 56.78 kips (252.66 kN), was characterized by the propagation of the existing web-shear cracks from the middle height of the specimen toward the bottom of the specimen. Major Eevnt 9 is characterized by the formation of additional flexure-shear cracks and the propagation of those cracks toward the bottom of the specimen. This was observed as the applied load was 59.55 kips (265.00 kN), loading to the north. Cracking associated with Major Events 1,8 and 9 is shown in Figure 3.28.
188.8.131.52 Propagation and Additional Web-shear cracking in Shear Wall Specimen 19
Major Events 10 and 11 correspond to the propagation of existing web-shear cracks and the development of new web-shear cracks in Shear Wall Specimen 19. At the north end, additional web-shear cracks formed at Load Point 1016, which corresponded to a base shear of 62.21 kips (276.85 kN). These cracks were extended through the wall and covering the center portion of the specimen almost to the base of the south end. A similar situation was observed at the south end of Shear Wall Specimen 19, specifically at Load Point 1073, corresponding to a base shear of 65.02 kips (289.33 kN). These diagonal cracks formed from the top to the bottom of the specimen and extended from the center portion of the specimen toward its north base. At this stage of the test, the south end of the specimen showed major damage, with cracking developing from the mid-height of the south end toward the bottom of it. The cracking pattern associated with Major Events 10 and 11 is shown in Figure 3.29.
184.108.40.206 Final damage in Shear Wall Specimen 19
Major Events 12 and 13 denote the final stage in the test of Shear Wall Specimen 19, and are associated with progressive damage at both ends of the specimen. This damage consisted of the propagation and formation of additional web-shear cracks in the specimen from the top to the bottom. At Load Point 1083, which corresponded to a base shear of 64.83 kips (288.47 kN), toe crushing was observed at the north end of the specimen. A similar situation occurred at the south end of the specimen at Load Point 1134, which corresponded to a base shear of 51.58 kips (229.52 kN0. At this stage, the specimen showed major damage with crushing of both compressive toes, along with a significant drop in in-plane stifness (about 14% of the initial stiffness) and strength. This observation is based on the reduction in slope of the hysteretic curve. The test was ended in Loading Cycle 10.
Figure 3.30 shows the damage in Shear Wall Specimen 19 at the end of the test. The significant amount and opening of the web-shear cracks and crushing of diagonal strut is shown in Figure 3.31 and Figure 3.32 respectively.
3.4.3 Load-Displacement Behavior for Shear Wall Specimen 19
The overall hysteretic behavior of Shear Wall Specimen 19 is shown in Figure 3.33. The maximum drift ratio for this specimen was about 0.49% in both directions. The test was stopped at in-plane displacements of 0.71 in (18.00 mm).
Summary, Conclusions and Recommendations
The purpose of this study was to evaluate the results of reversed cyclic load tests on 3 shear-wall specimens constructed with low-strength AAC (autoclaved aerated concrete). One shear wall specimen (SWS17) was designed to exhibit flexure-dominated behavior; the other two (SWS18 and SWS19) were designed to exhibit shear-dominated behavior.
The flexure-dominated specimen was constructed with vertically oriented, reinforced panels of low-strength AAC material. The objectives of this test were to examine the specimen's general hysteretic behavior, and to evaluate possible improvements in that behavior due to stainless steel spiral ties connecting the extreme-fiber elements to the remainder of the specimen.
The shear-dominated specimens were constructed with masonry-type units of low-strength AAC material. The specimens, with aspect ratios (height to plan length) of 0.71 and 1.34, had different arrangements of flexural reinforcement. The objectives of these tests were to examine the specimens' overall hysteretic behavior and validate the applicability to low-strength AAC shear walls, of proposed design provisions previouly developed based on shear-wall and assemblage tests with higher-strength AAC material. The overall hysteretic behavior of the specimens tested in this study was compared with the corresponding behavior of those specimens tested by Varela (2003). The results obtained with the proposed design provisions for the different capacities of the specimens tested in this study were compared with the corresponding mean values of those specimens tested by Tanner (2003).
In each test, quasi-static reversed cyclic loads were applied to each specimen, and the major events and overall hysteretic behavior were evaluated. After each test, overall damage was summarized; major events and hysteretic behavior were compared with predicted responses; and maximum drift ratios and displacement ductilities were assessed.
The study is the final facet of an extensive research project performed at the Ferguson Structural Engineering Laboratory of The University of Texas at Austin, using results for that and other testing laboratories (Tanner 2003, Varela 2003, Argudo 2003).
1) Previously proposed design provisions for nominal flexural capacity accurately predicted the capacity of flexure-dominated Shear Wall Specimen 17, and therefore are valid for low-strength AAC specimens as well as the higher-strength AAC specimens originally used to develop those provisions.
2) The maximum useful strain obtained in this study for low-strength AAC was less than the value of 0.003 reported by Tanner (2003). In fact, the maximum useful strain decreases with decreasing compressive strength, and was between 0.0015 and 0.002 for low-strength AAC. Because that capacity is governed by the mechanical characteristics of the reinfocement in all practical cases, regardless of the value of AAC max, previously proposed expressions for nominal flexural capacity are still valid. Previously proposed expressions for AAC modulus as a function of specified compressive strength are also valid.
3) Stainless steel spiral ties, used to connect the end U-blocks of Shear Wall Specimen 17 to the vertical panels comprising the rest of the wall, significantly reduced deterioration of the compression toes of that specimen under cycles of reversed cyclic load. The specimen achieved in-plane lateral drift ratios of 0.65% and lateral ductilities of 5 in both directions.
4) Previously proposed design provisions for web-shear capacity accurately predicted the capacity of shear-dominated Shear Wall Specimens 18 and 19, and therefore are valid for low-strength AAC specimens as well as the higher-strength AAC specimens originally used to develop those provisions.
5) The shear capacity of Shear Wall Specimens 18 and 19 was governed by crushing of the diagonal strut, at a drift ratio of 0.37 % (loading to the north) for Shear Wall Specimen 18 and 0.26% (loading to the north) for Shear Wall Specimen 19.
6) The overall hysteretic behavior of the shear-dominated specimens (SWS18 and SWS19) was characterized by a sudden degardation in stiffness after web-shear cracking and showed a behavior consistent with that of the shear-dominated specimens tested by Varela(2003). The maximum drift ratio obtained for Shear Wall Specimens 18 and 19 were 0.48 and 0.49 in both directions respectively.
7) The ductilities and drifts obtained in this study are consistent with those obtained by Varela (2003) for flexure-dominated shear walls of higher-strength AAC material, in spite of the lower maximum useable strain of the low-strength AAC. Therefore, the R and C values proposed by Varela (2003) are valid for low-strength AAC material as well.
8) Based on the close agreement obtained between observed and predicted values for capacities and stiffnesses, the analytical models used to represent the behavior of shear-dominated and flexure-dominated specimens, constructed with AAC material of medium and high compressive strength, are also applicable to specimens constructed with AAC material of low compressive strength.
5.3 RECOMMENDATIONS FOR FUTURE WORK
1) Additional testing should be performed on AAC shear walls with openings. Such testing would provide information about the behavior (limit states) of AAC walls with openings compared to the capacity predictions of current design provisions.
2) Additional work should be performed to develop strut-and-tie models for AAC walls. These models would offer the possibility of simplified design approaches by comvining web-shear cracking, flexure-shear cracking and crushing of the diagonal strut, in a single design model.
3) Additional research should be performed on ways to use grouted regions within AAC shear walls to increase their resistance to flexural compression, to crushing of the diagonal strut, and perhaps to sliding. Possible failure at the interface between the AAC material and the grout can be avoided using spiral ties. The purpose of this research would be o improve the strength and ductility of AAC shear walls.
4) Additional research should be conducted on the behavior and design of AAC infill panels in frames of structural steel or reinforced concrete. Such infills could increase the strength, stiffness and energy dissipation capacity of framed structures, in retrofit as well as new construction.
5) Additional research should be conducted on increasing the sliding-shear capacity of AAC shear walls. This would result in AAC structures with higher factors of safety against sliding in zones with large spectral ordinates.
Design Provisions for Reinforced AAC Shear
A.1 DESIGN OF AAC SHEAR WALLS
Appendix A was originally developed as part of the PhD dissertation of Tanner (2003). It is included here so that the reader will be able to see the context in which the design provisions discussed in this thesis were originally proposed.
A suite of 14 AAC shear wall specimens, with aspect ratios (height of the point of load application divided by the plan length) from 0.6 to 3, has been tested at the University of Texas at Austin. The behavior of each shear wall may be shear- or flexure-dominated. The shear-dominated specimens were heavily reinforced in flexure using external reinforcement. The flexure-dominated specimens were lightly reinforced in flexure. The test setup is shown in Figure A.1.
Physical details for each specimen are presented in Table A.1. The number after the supplier's name identifies in which shipment the AAC material arrived.
Results from a suite of 12 shear-wall tests performed by Hebel (Germany) provide additional information. Each of those walls measured 8.2 ft (2.5 m) long, 8.2 ft (2.5 m) tall and 9.5 in. (0.24m) thick. The aspect ratio of each specimen is 1.0. The test set up is shown in Figure A.2. Additional physical details for each Hebel specimen are presented in Table A.2.
In the Hebel tests, axial load was applied using uniformly spaced, external post-tensioning rods. This axial load was monitored and was kept constant. Two additional 1 in. (25 mm) diameter rods on each side of the wall, with initial pre-tension less than 0.5 kip (2kN), were used as external reinforcement. As the wall reinforcement on the tension side. The rods on the compressive side of the wall are not initially post-tensioned, so the force in them does not decrease as the force in the tension rods increases. Increasing the force in the tension rods without decreasing the force in the compression rods is equivalent to applying an additional compressive axial load to the wall. Therefore, the axial load in the Hebel specimens changed as the lateral load changed. The axial load used to evaluate the behavior of the Hebel specimens at each state is the initial axial load (including weight of loading equipment) plus the summation of tensile forces in the rods at that state.
A.1.1 Web-shear Cracking
Using additional data points determined at UT Austin between November 2001 and August 2002, the relationship between splitting tensile strength and "1386 density" presented in Equation (A.1) has been replaced by .... As discussed in this section, that difference in splitting tensile strength is less a few percent, and the actual change in computed values of Vaac is quite small.
This section is dedicated to explaining the changes. The form of the equation for Vaac will stay the same, with only slight changes in the external coefficients. In the following section, the derivation of the equation for web-shear cracking is reviewed.
The shear strength of the AAC shear-wall specimens was initially predicted using Equation (A.6). The ratios of observed to predicted capacities, shown in Table A.3, indicated that the ratio of observed strength to predicted strength of Shear Wall Specimen 1 (UT Austin) is significantly greater than for the other specimens, and can be considered an anomaly with respect to the rest of the tests. The remaining specimens show lower observed than predicted strengths, indicating that Equation 9A.6) is unconservative.
To further evaluated the effects of mortared head joints, the AAC shear-wall tested at UT Austin and by Hebel (Germany) are divided into two groups: those with fully mortared head joints, and those with unmortared head joints. The range of ratios of observed Vaac to predicted Vaac is 0.54 to 0.1.29 for the fully mortared specimens, and 0.33 to 0.51 for the partially mortared specimens. For the specimens with fully mortared head joints, the mean ratio of observed to predicted Vaac is 0.70, with a coefficient of variation of 17%. For the specimens with unmortared head joints, corresponding values are 0.46 and 13%.
These data can be plotted in Figure A.3 and Figure A.4. In each figure, the mean ratio of observed capacity to that predicted using the theoretical Equation (A.6) is represented by a solid horizontal line. Also plotted on each figure is the normal distribution with the same mean and COV as the test data. The lower 10% fractile of that distribution, shown by a dashed horizontal line, has a value of 0.55 for the fully mortared specimens and 0.38 for the partially
Equation (A.6) was therefore reduced so that it would correspond to the lower 105 fractiles of the ratios of observed to predicted capacities. In carrying out that reduction, fully mortared and partially mortared specimens were considered separately. Equation (A.6) was multiplied by 0.55 to obtain proposed Equation 9A.1) for fully mortared specimens. In the same way, Equation (A.6) was multiplied by 0.38 to obtain proposed Equation (A.2) for partially mortared specimens.
The predicted Vaac using Equation (A.1) and Equation (A.2) are presented in Table A.5 and Table A.6,
Table A.6 shows the prediction of capacity for all specimens that exhibited web-shear cracking. Ratios of observed Vaac versus predicted Vaac using Equation (A.1) and Equation (A.2) based on the tested compressive strength are presented in Figure A.5. In that figure, a solid diagonal line represents perfect agreement between observed and predicted shear capacities. The proposed equations are very close, or have slight errors in the direction of conservatism, for the specimens tested. If the ACI 318-02 equation for web shear cracking is used directly for AAC, the predicted capacity is greater than that observed, and hence unconservative. This is also true if the ACI 318-02 equation for web shear cracking is used with equivalent expressions for the tensile strength of concrete and for AAC. The web-shear cracking capacitywill be further reduced by using the specified compressive strength rather than the tested compressive strength. These results for the specimens tested at UT Austin are presented in Figure A.6. The one data point where the observed Vaac falls below the predicted Vaac is the Two-story Assemblage Specimen where the tested compressive strength fell below the specified compressive strength.
A.1.2 Flexure-Shear Cracking for AAC Shear Walls
A flexure-shear crack begins as a horizontal crack at a height of about one-half the plan length of the wall above the base of the wall, and then propagates diagonally through the center of the wall, as shown in Figure A.7.
Based on experiements with reinforced concrete shear walls, the controlling horizontal crack develops at a height of about lw/2. Threrfore, the moment at the crack, Mflcr is:
A.1.3 Crushing of the Diagonal Strut
An AAC shear wall can transfer load through the formation of a diagonal strut. The resultant of the applied lateral load and vertical forces acting on a wall is transferred along a diagonal strip in the wall (Figure A.13). The compressive force transfeered along the diagonal strut is equilibrated at the base of the wall by the frictional resistance and by the vertical component of the compressive force in the diagonal strut. AAC shear walls with high axial loads can fail by crushing of this diagonal strut.
Crushing of the diagonal strut will occur in an AAC shear wall when the compressive stress in the strut exceeds the compressive strength of the AAC. Figure A.14 shows the external forces acting on an AAC shear wall due to in-plane shear and axial load.
Diagonal crushing can be predicted using a strut-and-tie model consisting of two element: a diagonal compression strut (Fstrut); and a tension tie-down force (T). The compressive force in the diagonal strut is the resultant of the vertical tie--down forces and the applied horizontal load. Because the system is statically determinate, the vertical component is the summation of the force in the tie-down rods, and the horizontal component is the applied lateral load (V).
Equation (A.19) represents the horizontal force (V) at crushing based on equlibru\ium of horizontal forces at the base of the diagonal strut. The derivation can be shown in Equation (A.130 to Equation (A.18). The limiting force in the diagonal strut is based on an uniform compressive stress acting over the smallest area of the strut, as shown in Equation (A.13). The maximum applied lateral load is related by geometry to the force in the strut. Likewise, the minimum width of strut can be related to the horizontal width of the diagonal strut. By substitution, the lateral load of Equation (A19) can be expressed in terms of the wall geometry and horizoontal width of the strut (see Equation (A.16) and Equation (A.17)).
Shear Wall Specimen 1 (UT Austin) comfirmed this proposed model for crushing of the diagonal strut. Minor spalling occurred at the toe at a load of 152 kips (676 kN), and major spalling, at a load of 167.6 kips (745 kN). The observed horizontal width of the diagonal strut was approximately one-quarter of the plan length. Using Equation (A.19), crushing of the diagonal strut for Shear Wall Specimen 1 was predicted at a lateral load of 185.1 ki[ps (823 kN). The ultimate load was 90% of the load predicted by the model for crushing of the diagonal strut. Since, the model for crushing of the diagonal strut was unconservative in this case, it is multiplied by a factor of 0.9. Equation (A.20) incorporates this factor and a width of the compression strut of 0.25lw. The results of the predicted lateral load at crushing of the diagonal strut, for and assumed strut width of one-quarter of the plan length, are present along with the ultimate lateral load in Table A.9.
In the remaining shear wall specimens crushing of the diagonal strut was avoided by limiting the axial load. The validity of Equation (A.20) was indirectly determined by avoiding crushing. In Shear Wall Specimen 13, the maximum lateral load was higher than the proposed equation for the design provisions without observing crushing of a diagonal strut. One reason for the discrepancy is that the assuemd width of the diagonal strut of one-quarter of the plan length of the wall is no longer valid. The aspect ratio of Shear Wall Specimen 13 is 2. Since the model was adequate for walls with aspect ratios less than 2, that aspect ratio is used as an upper limit to the proposed Code equation.
A.1.4 Sliding Shear Capacity
An AAC shear wall of horizontal panels or masonry-type blocks exhibits a bed-joint crack when the shear stress on the bed joints exceeds the interface shear capacity, v (Figure A.18). An AAC shear wall subject to sliding shear across a horizontal bed joint is presented in (Figure A.16). After the crack forms the shear is resisted by the vertical reinforcement and frictional forces due to the axial load.
Sliding shear resistance is the product of the coefficient of friction across an interface, and the force acting perpendicular to that interface. This mechanism is referred to in ACI 318 as "shear friction." This resistance can come from reinforcement crossing the interface and applied axial load.
In the traditional "shear friction" mechanism, sliding over a rough joint causes one section of the crack to lift upwards; this result in yielding of the vertical reinforcement, which provides additional clamping force. Under reversed cyclic loading of AAC, the roughness of the bed joints can decrease, and resistance to sliding shear is provided by dowel action of reinfocement crossing the bed joints. This contribution to Vss is the area of the reinforcement perpendicular to the crack and the shear resistance of the bars, 0.6 fy. This contribution to the sliding shear mechanism is shown in Figure A.18.
Frictional resistance is the second component of resistance due to sliding shear. Figure A.19 is a free-body diagram showing the horizontal equilibrium due to frictional forces.
In subsequent specimens, the clamping force N was determined such that the shear capacity will be limited by web-shear cracking or flexure-shear cracking, rather than bed-joint sliding. Sliding shear was avoided in 12 out of the remaining 14 specimens; it was observed in Shear Wall Specimen 4 and the Two-story Assemblage Specimen. Since the specimens were designed to avoid sliding shear, sufficient dowels were placed to ensure that Vss was significantly greater the Vaac. In four specimens, Vmax was greater than Vaac. Shear Wall Specimen 3 and Shear Wall Specimen 5 were both overdesigned in sliding shear. The load did not reach the sliding shear capacity because the specimen capacities were limited by distributed web-shear cracking. Shear Wall Specimen 4 and the Two-story Assemblage Specimen can be used to determine the effectiveness of Equation (A.22).
The hysteretic behavior for the Two-story Assemblage Specimen is shown in Figure A.20. The total base shear and sliding shear capacity for the specimne versus Load Point is presented in Figure A.21. The design sliding shear capacity is presented for the contribution of axial load and dowels (Equation (A.22)) and the contribution of axial load only. A coefficient of friction of 1.0 was used since the sliding plane occurred between the vertical panels and the leveling bed mortar. The entire axial load was applied through gravity, therefore, the axial load remained constant throughout the test. In this specimen the longitudinal steel and dowels contribute significantly to the capacity for several cycles. Damage around the dowels began at Load Point 677 and continued throughout the test. Each loading cycyle was accompanied by increasing damage. The cumulative damage at each cycle is accompanied by a continually decreasing base shear, as shown in load points above 800 in Figure A.21.
Sliding was observed in two adjacent panels in Shear Wall Specimen 4. A horizontal crack formed along the bed joint between the second and third courses. This crack formed in three stages, corresponding to Load Points 634, 717 and 764. The final crack propagation occurred after the maximum base shear was reached. A graph of base shear versus Load Point for Shear Wall Specimen 4 is shown in Figure A.22. Since the sliding occurred between panels, a coefficient of friction of 0.8 was used to predict the capacity. The applied base shear increased beyond the sliding shear resistance for the level of axial load that was applied to the specimen. Several diagonal cracks formed at the compression toes of the walls. Spalling between these cracks occure\red at Load Point 871.
The axial load consisted of three portions: gravity load from loading equipment; load applied through the load maintainer; and post-tensioning force in the rods. The pressure in the load maintainer system was checked during testing. In did not change, nor did the contribution of axial load due to gravity. Any decrease in axial load would therefore have to have occurred due to a loss of post-tensioning. This was observed in the spalling of the compression toe that occurred at Load Point 871. The loss of post-tensioning decreased the applied axial load and thus decreased the sliding shear capacity.
The measured axial load capacity of Figure A.23 includes the unchanged axial load and the measured force in the external rods. As the base shear increases, a slight increase is also observed in the axial load (see Load Point 1080 through 1110). This is the increase in load in the axial rods caused by the in-plane rotation of the wall about its compression toe. At later load points, at points of zero base shear the force in the rods decreases due to toe crushing. This can be observed in the difference between measure axial loads at two points where the base shear is zero. For example, at Load Point 830 the measured axial load is 91 kips (405 kN); at Load Point 890 it decreases to 87 kips (387 kN); and at Load Point 960 it further decreases to 82 kips (365 kN).
Flr load points beyond 700 the base shear capacity decreases. This was also observed in the Two-story Assemblage Specimen. This is a further indication that as damage increases the effectiveness of the dowel action decrease. As the damage increases, the resistance provided by bearing on the dowel is reduced. For this reason, the proposed code language conservatively neglects the contribution of the dowels as shown in Equation (A.23).
Structures with small axial load may have low sliding shear capacity. In these cases the interface shear strength between AAC and thin-bed mortar may be used. Based on the direct shear tests performed at UT Austin, the average interface shear strength between AAC and thin-bed mortar was 64 psi (441 kPa), with a COV of 44%. A lower 5% fractile is proposed, for design, reducing the interface shear strength to 17 psi (117 kPa). This value is conservative compared to test results of 45 psi (310 kPa) to 82 psi (565 kPa).
The measured axial load in Figure A.23 does not include the tensile forces in the internal reinforcement. Although those forces were not measured, they can be estimated based on flexural calculations. The wall instrumentation indicates that the longitudinal reinforcement in the wall had yielded at the bed joint where sliding occurred. When the lateral load is removed and the bed-joint gap closes, the bars will be subject to compression. Based on an assumed debonded bar length, the compressive forces can be setimated. The solid blue line in Figure A.24 shows the revised axial load considering compressive stresses in longitudinal reinforcement.
A.1.5 Nominal Flexural Capacity
The nominal flexural capacity of AAC shear walls can be determined based on equilibrium of a cross section. Using the proposed design provisions, the nominal flexural capacity of AAC shear walls can be predicted using conventional flexural theory. The compressive zone is determined based on a linear strain relationship, using a maximum useful compressive strain in the AAC of 0.003 (RILEM 1993 and Section 4.3.1), and an equivalent rectangular stress block whose height is 0.85, and an equivalent rectangular stress block whose height is 0.85 , and whose depth is, where =0.67 (Figure A.25). The value of is selected to maintain equilibrium between the equivalent stress block and triangular compressive stress distribution based on tested stree-strain results of Section 3.6.1.
Observed versus predicted nominal flexural capacities can be compared fle flexure-dominated Shear Wall Specimen 14a, 14b, 15a and 15b. During the test of Shear Wall Specimen 13 and Shear Wall Specimen 16, the actuators used to apply the constant axial load inadvertently reached the end of their travel. As increasing lateral drifts were applied, axial load on the wall inadvertently increased. To successfully interpret those test results, the probable axial load applied to the walls was back-calculated from the predicted flexural capacity, removing those two tests from consideration for verifying observed versus predicted flexural capacity.
The nominal flexural capacity was calculated using a steel yield strength of 75 Ksi (490 MPa), based on mill reports, along with the assumptions of 8.8.2. The ratios of observed to predicted strength range from 1.11 to 1.29, with an average of 1.19 and a COV of 5.8%. A refined analysis was performed considering strain hardening using RCCOLA (RCCOLA). The effect of srain hardening will increase the nominal flexural capacity as shown in the results of Table A.11. With this refinement the range of observed to predicted nominal flexural capacity ranges from 0.95 to 1.13. The average is 1.03 with a COV of 6.2%.
A.2 SPECIAL PROVISIONS FOR VERTICAL PANEL CONSTRUCTION
AAC panels oriented vertically have potential planes of failure along continuous head joints. These cracks may be attributed to shrinkage or weak joints, where the thin-bed mortar is not in contact with both panel faces. The presence of vertical cracks can change the behavior of a shear wall specimen. The observance of this behavior in Shear Wall Specimen 2 will be discussed then theoretical and design methodologies will be presented in Sections A.2.1 and A.2.2.
In Shear Wall Specimen 2, two vertical cracks formed prior to testing. Shortly after flexural cracks formed another two vertical cracks formed and separated the wall into smaller sections. The initial cracks are indicated by gray lines and the cracks formed during testing are indicated by black lines in Figure A.26. The first diagonal crack formed at a load of 55.6 kips (247 kN). As the load increased, additional vertical and diagonal cracks formed in the specimen (Figure A.27).
A.2.1 Prediction of Flexural and Shear Capacities for AAC Shear Walls with Vertically Oriented Panels
In the case of monolithic behavior, the wall behaves as a cantilever (see Figure A.28). In the case of individual panels, the stiffness of the loading beam is large compared to a single panel, and the loading beam restrains the wall at the top (Figure A29). If the wall behaves monolithically, the shear capacity will remain the same as presented in Section A.1, and the flexural design will be conventional. If the panels are separated by vertical cracks at the head joints, however, the behavior will change. That is the subject of this section.
The most critical case would be panels with vertical cracks at every section. The flexural capacity can be predicted based on the sum of the capacity of the individual panels. An interaction diagram for a single panel can be calcaulated and the flexural capacity of each panel can be determined based on the axial load in the respective panel; a value that depends on the forces acting on the wall. The lateral load will produce a series of axial loads in each panel that vary linearly based on the wall geometry. Teh applied axial load per lanel will be the total axial load divided by the number of panels (see Figure A.30).
If the net axial load applied to each panel is within the straight-line portion of the interaction diagram for a single panel, the total wall capacity will be the capacity at the axial load in a single panel, multiplied by the number of panels:
If the wall behaves as individual panels, the aspect ratio of piece becomes large; each panel bahaves as a beam subject to compressive and lateral loads. The shear capacity in this condition can be predicted using the shear equations for beams presented in Section 4.5.
A.2.2 Verification of Shear Capacity for Vertical-Panel Shear Walls Tested at Ut Austin
The application of the individual panel design equations and the monolithic wall equations for Shear Wall Specimen 2 is presented in Figure A.31. The base shear at which cracking occurred was 55 kips (245 kN), and the maximum base shear was 92 kips (410 kN). The design equations are much more conservative than the wall behavior.
Several conditions can increase the performance of a head joint between vertical panels:
a) Cleaning and wetting the panel face prior to application of the thin-bed mortar improves the adhesion.
b) Applying mortar to both faces of the vertical joint improves the mortar coverage at the joint.
c) Clamping adjacent panels applies pressure and improves the joint quality.
In Shear Wall Specimen 2 the panel faces were prepared and pressure was applied perpendicular to the joint, parappel to the plane of the wall. Initially, the joints were not mortared on both faces. After a lack of coverage was observed in several joints, the panel was removed, cleaned and re-installed with mortar applied to both faces of the joint. This procedure was applied thereafter. The joint was clamped at the base (using one clamp on each wall face) and at the top (using one clamp at the centerline of the wall).
In the remaining specimens constructed of vertical panels (Shear Wall Specimens 15, 16 and the Two-story Assemblage Specimen), vertical cracks were not observed. In each case the three previous construction recommednations were used. Pressure was applied to th ejoint using 4 clamps, one clamp on each wall face, both at the bottom and top of the wall.
In these specimens, vertical cracks at the joints were not observed until the end of the test when the wall stiffness was reduced due to prior cracks. Furthermore, the cracks left at least three panels joined together. For this construction type, the proposed design recommedation is to relax the individual panel requirements to groups of three panels connected together. The changes to the flexure and shear design capacities are presented in Figure A.32. Equation (A.3) to predict web-shear cracking was used for panel groups with an aspect ratio less than 2.
A.2.3 Special Provisions to Avoid Longitudinal Cracking at the Location of Vertical Reinforcement
In each of the flexure-dominated specimens vertical (longitudinal) cracks formed along the grouted cores and the surrounding AAC. In the following sections the observed load at which these cracks formed is presented, along with two analyses to determine if the cracks occurred before yielding of the flexural reinforcement. The effect of these longitudinal cracks is presented, followed by design recommendations intened to prevent their formation.
A.2.4 Formation of Cracks along Longitudinal Bars in AAC Shear Walls
The base shears at which cracks formed along longitudinal reinforcement formed are presented in Table A.12. The base shear at which the first and second cracks formed along the vertical reinforcement is presented in Column 2 of that table. No second observed vertical crack data are presented for Shear Wall at the expected flexural capacity (nominal capacity increased by steel overstrength) is presented in Column 3.
The ratios of base shear at the observed crack to the base shear at the expected flexural capacity range from 0.74 to 1.20, with an average of 1.02 and a COV of 16%. Longitudinal cracks were observed in three specimens at 74% to 84% of the expected flexural capacity. The ratios of base shear at cracking to expected flexural capacity, along with a corresponding normal distribution, are shown in Figure A.33. As shown in that figure, it is highly probable that an AAC shear wall will reach between 74% and 84% of its expected flexural capacity in a moderate to strong earthquake, and therefore highly probable that such longitudinal cracks would form.
For lower base shears, a similar analysis can be performed. The results of Table A.12 are reproduced based on nominal moment capacity (rather than expected), and are presented in Table A.13. In this case the ratios of base shear at longitudinal cracking to base shear at nominal capacity range from 0.84 to 1.42, with an average of 1.2 and a COV of 15.5%. These data are illustrated graphically in Figure A.34. The ratio of 1.0 between base shear at longitudinal cracking to base shear at nominal flexural capacity, corresponds to a 16% lower fractile. A 5% lower fractile corresponds to a ratio of 0.88. Based on these results, 5% of shear walls would exhibit longitudinal cracking at the factored nominal flexural capacity. To further determine if vertical cracks would occur at service loads, analyses were performed to determine if the cracks formed prior to yielding, and are presented in the following section.
A.2.5 Analysis to Determine if Longitudinal Cracks Formed Prior to Yielding
Additional analysis was performed to determine if longitudinal cracks formed before or after the vertical reinforcement yielded. If the vertical cracks formed prior to yielding, then those cracks might also be present in walls at factored design loads. If the vertical cracks formed after yielding, it can be assumed that they would occur only during overloading beyond the nominal capacity.
Strain was measured by three strain gages on the longitudinal reinforcement at each end of the wall. If one strain gage indicated strains beyond yield and another strain gage indicated strains near but not exceeding yield, this was assumed to denote yielding. The base shear and load points at the formation of longitudinal cracks in each specimen, while loading to the south and to the north, are recorded in Column 2 of Table A.14. In Shear Wall Specimen 13, strain gage data were not available; for this reason, in Column 2 both the South and North loading directions are labeled "NA." The base shear and load points at the yielding of the flexural reinforcement are presented in Column 3. Since load points are assigned in ascending order, the first event (either longitudinal cracking or yielding of longitudinal reinforcement) has the lowest-numbered load point. The event that occurred first for each loading direction is presented in Column 4. If the load-point numbers did not vary by more than 5, it was assumed that longitudinal cracking occurred simultaneously with yeilding of flexural reinforcement, and was therefore associated with that yielding. For example, in Shear Wall Specimen 14a while loading to the south, longitudinal cracking was observed at Load Point 542, and the longitudinal reinforcement was determined to have yielded at Load Point 539. Since these load points do not vary by more than 5, it was concluded that the longitudinal cracking and yielding of the reinforcement occurred simultaneously, as indicated in Column 4. Finally, the ratio of base shear at longitudinal cracking to base shear at yielding is presented in Column 5.
In four cases, yielding occured before longitudinal cracking; and in two cases, it occurred afterwards. In the remaining cases these events probably occurred simultaneously. In both cases where the flexural reinforcement yielded after longitudinal cracks were observed, the ratio of base shear at formation of longitudinal cracking to base shear at yielding was also less than 1. This further supports the conclsuion that if #5 bars are used in 3 - in.grouted cores, longitudinal cracks may form prior to yielding of the flexural reinforcement. The ratio of base shear at longitudinal cracking to base shear at yielding is less than 1.25 for all of the specimens, which indicates that longitudinal cracks will probably form prior to reaching the nominal flexural capacity considering a strain hardening factor of 1.25. This analysis does not consider the height at which the vertical crack formed. If the crack formed at a height of 48 in. (1.2 m) the stress in the reinforcement could be significantly below yield. The impact of crack height is considered in s separate analysis.
An additional analysis was performed to estimate the stress in the flexural reinforcement at longitudinal cracking, using elastic flexural stresses calculated based on a cracked transformed section (Table A.15). The applied base shear was converted to an applied moment at the location of the crack by multiplying by the height of the wall minus the crack height. The stress in the lonitudinal tensile reinforcement was computed using Equation (A.26). The contributions from the axial load are not presented in Table A.15 because they were less than 2 ksi (14 MPa). The distance from the neutral axis to the centroid of the tensile reinforcement is denoted by yAs, the modular ratio between steel and AAC is denoted by n; and the cracked transformed moment of inertia is denoted by I. The results indicate that in 6 of the 11 cases, calcalated stresses at longitudinal cracking exceeded the expected yield strength of 75 ksi (10.9 GPa). This indicates that approximately half of the vertical cracks occurred prior to or simultaneously with yielding of the flexural reinforcement.
A.2.6 Implications of the Formation of Longitudinal Cracks
The above evaluations show that longitudinal cracks are highly probable in real AAC shear walls subject to lateral loads. This section is devoted to explaining the probable consequences of those cracks and providing design recommendations for preventing them.
Cracks along reinforcement in a grouted core are inherently undesirable, because they provide an opportunity for air and water to enter the core, and thereby increase the probability of conrrosion of that reinforcement. Longitudinal cracks along the height of the wall, combined with horizontal cracks, can cause the end blocks to spall and crush sooner than in otherwise identical walls without longitudinal cracks (Figure A.35). Longitudinal cracks can also lead to buckling of the longitudinal reinforcement in the compression toe (Figure A.36).
As the load is reversed, the previously buckled longitudinal reinforcement may fracture, effectively reducing the wall's flexural capacity to zero. Examples of the undesirable consequences of loss of the compression toe are shown by Shear Wall Specimen 15b and Shear Wall Specimen 16.
Resistance to cracks along longitudinal reinforcement could be increased. Longitudinal splitting cracks could be prevented by increasing the size of grouted core or decreasing the bar diameter. This is equivalent to limiting the ratio of area of the longitudinal reinforcement to area of core (aera ratio).
The area ratio of a #5 (17 mm) bar in a 3-in. (76 mm) diameter grouted core (4.4%) was observed to produce splitting along longitudinal bars in plastic hinge zones. This is inherently undesirable for AAC shear walls. Such cracking not been observed with #4 bars in 3 - in. grouted cores, even at splices. A #4 (12 mm) bar in a 3 in. (76 mm) core corresponds to an area ratio of 2.8%. For that reason, the proposed design provisions for AAC masonry and reinfoced AAC panels limit the maximum ratio of the area of reinforcement to the area of the grouted core containing that reinforcement. to 3% in plastic hinge zones.
A.2.7 Analysis of Maximum Permissible Area Ratio if Longitudinal Reinforcement Remains Elastic
Area ratios of reinforcement up to 4.5% are permitted, provided that radial (splitting) stresses can be limited by limiting the bond stress, which in turn means limiting the shear. The formation of radial stresses is explained in Section 8.8 of this dissertation, and briefly reviewed here.
After the initial adhesion between the reinforcement and concrete is broken, load is transferred from deformed reinforcement to the surrounding concrete or grout by the deformations (lugs). The axial component of the force transferred by the lugs to a vertical core is the difference in force in a section of vertical reinforcement. The associated radial component of that force also acts on the sourrouding grout (Figure A.37). The resultant forces generally act at about 45 degrees to the axis of the reinforcement, so that the resultants of the radial and axial component of the forces are equal. The radial forces generated per length of the bar equal the change in force in the bar over that same length. The pressure generated by the radial forces in the longitudinal bar can be determined by dividing the raidal forces by the product of the circumference of the deformed bar and the length of the section of the bar, as shown in Figure A.37. The diameter of the lonitudinal bar is denoted by Dbar.
For design convenience the bond stress can be expressed as a function of shear as shown in Equation (A.27). This relationship is valid in cases where the bond between grout and reinforcement remains intact. Generally bond is broken after the reinfocement yields, therefore this development does not apply to cases where a plastic hinge may form. For practical reasons this analysis based on Equation (A.27) is limited to out-of-plane loading. Since the resultant force acting on the lugs acts at about 45 degrees, the radial stresses, are also equal to the bond stress, u, as shown in Equation (A.28).
These raidal forces cause splitting tensile stresses along a section through the wall at the center of the grouted core. Because the AAC has only about 15% of the splitting tensile strength of the grout, its tensile strength is neglected. A uniform distribution of splitting stresses across any section through the diameter of the grout core is assumed as shown in Figure A.38a. Since the radial stresses are symmetric about the centerline of the core (Figure A.38a), the net resultant of those radial stresses perpendicular to the centerline is zero. The splitting tensile stresses are resisted by the splitting tensile capacity of a section of grout, whose area is the length of grout shown in Figure A.38 b, multiplied by the length of a section. The resistance to the splitting tensile stresses is expressed in Equation(A.29). The resistance is increased by increasing the diameter of the core, decreasing the diameter of the bar, or increasing the tensile strength of the grout.
The uniform splitting stress across a section of grout as shown in Figure A.38a is calculated by integration. Figure A.39 a shows the radial stress acting at the interface between the bar and grout. The vertical comonent of stress which corresponds to a uniform splitting stress is calculated using geometry for a differential section of the arc, ds (Figure A.39b). Integrating this expression for the vertical component of force between angles of 0 and 3.1415926... yields the expression for the total force generated by the splitting stress shown in Equation (A.30). If the resultant of the uniform splitting stress shown in Equation (A.30). If the resultant of the uniform splitting tensile stress is set equal to the total force supplied by the resistance of the grout (Figure A.38), Equation (A.31) is generated. The splitting tensile strength, is expressed in terms of the the bond stress in Equation (A.32).
Based on this analysis, for reinforcement in the elastic stress range, the acting splitting tensile stress can be calculated. In such a case the area ratio of longitudinal steel may be increased beyond the proposed value of 3% for the design provisions of Section A.2.8. These proposed design provisions permit area ratios of longitudinal steel to grouted core up to 4.5%, provided that the splitting tensile stress generated in the core is less than the available splitting tensile strength. A detailed example of these calculations is presented in a design example involving walls subject to out-of-plane loading. The proposed design provisions in ACI 318-02 Code language are as follows:
A.2.8 Analysis of the Maximum Permissible Area Ratio in a Plastic Hinge Zone
If the reinforcement is located in a plastic hinge zone, compatibility of strains no longer exists between the reinforcement and the surrounding grout, and the splitting tensile stress cannot be determines using Equation (A.32). Based on the cracking observed along the flexural reinforcement in the flexure-dominated specimens (Section A.2.4), the proposed design provisions limit the area ratio to 3% in areas where a plastic hinge may form.
A.3 DESIGN EXAMPLES
A.3.1 Design of an AAC shear wall
Design the following two-story AAC shear wall. Material properties, factored loads, and geometry are:
A.3.1.1 Flexural capacity
Determine factored bending moment at the base of the wall:
M = 18000 (15)(12) + 18000(7.5)(12) = 4860000lbs - in.
Determine flexural capacity at the base of the wall. Assume flexural reinforcement at wall ends only, equal to 1# 4 bar, located 24 in. from the wall ends.
A.3.1.2 Shear capacity
Determine factored shear force and axial force at the base of the wall: ...
A.3.2 Design an AAC Shear Wall for Out-of-plane loads
A.3.2.1 Flexural capacity
Determine acting moment:
Perform an analysis to check the bond stress. In the case of out-of-plane loads the reinforcement in the wall does not yield and no plastic hinge forms. In this example, the classical bond stress analysis shown in the example can be used.
Check bond stress:
Determine if reinfocement is yielding:
Mn = 0.9*85, 700 lb-in = 77130 lb-in. >Mu=66000 lb-in, reinforcement will not be yielding. Since reinforcement will not be yielding consider case where bond remains intact and express bond stress as a function of shear.
Determine shear and bond stress along the length of the wall. Based on the bondstress determine the splitting tensile stress in the wall and compare to the splitting tensile strength of the grout.
A.3.2.2 Shear capacity
Determine factored loads and maximum shear force for a single panel.
ACI 523.5 R-xx Guide for using Autoclaved Aerated Concrete Panels
Appendix B consists of the first several draft chapters in a Guide for usng Autoclaved Aerated Concrete Panels, under development in ACI Committee 523A, Cellular Concrete. Much of the material in that draft chapter was extensively rewritten for inclusion in the MS thesis of Argudo (2003). It is presented here to give the reader basic background information on AAC.
B.1.1 Definition of Autoclaved Aerated Concrete
Autoclaved Aerated Concrete (AAC) is a low-density cementitious product of calcium silicate hydrates in which the low density is obtained by the formation of macroscopic air bubbles, mainly by chemical reactions within the mass during the liquid or plastic phase. The air bubbles are uniformly distributed and are retained in the matrix on setting, hardening, and subsequent curing with high-pressure steam in an autoclave, to produce a cellular structure (Figure B.1). Material specifications for this product are prescribed in ASTM C 1386.
B.1.2 Typical Mechanical and Thermal Characteristics of AAC
In Table B.1, typical mechanical and thermal characteristics of AAC are compared with those of conventional concrete, including conventional concrete made with lightweight aggregates. AAC typically has one-sixth to one-third the density of conventional concrete, and about the same ratio of compressive strength, making it potentially suitable for cladding and infills, and for bearing-wall components of low-to medium-rise structures. hermal conductivity is one-sixth or less that of concrtee, making it potentially energy-efficient. Its fire rating is slightly longer than that of conventional concrete of the same thickness, making it potentially useful inapplications where fire resistance is important. Because of its internal porosity, AAC has very low sound transmission, making it potentially useful acoustically.
B.1.3 Historical Background of AAC
AAC was first produced commercially in Sweden, in 1923. Since that time, its production and use have spread to more than 40 countries on all continents, including North America, Central and South America, Europe, the Middle East, the Far East, and Australia. This wide experience has produced many case studies of use in different climates, and under different building codes.
In the US, modern uses of AAC began in 1990, for residential and commercial projects in the southeastern state. US production of plain and reinforce AAC started in 1995 in the southeast, and has since spread to other parts of the country. A nationwide group of AAC manufacturers was formed in 1998 as the Autoclaved Aerated Concrete Products Association. This Guide is an effory by the AAC technical community, including manufactures, designers and researchers, to propose national design guidelines that could later be developed into code provisions.
B.1.4 Applications of AAC Panels
AAC can be used to make unreinforced, masonry-type units, and also factory-reinforced floor panels, roof panels, wall panels, lintels, beams, and other special shapes (Figure B.2). These elements can be used in a variety of applications including residengtial, commercial and industrial construction. Reinforced floor and roof panels can be efficiently used to provide the horizontal diaphragm system while supporting the necessary gravity loads.
B.1.5 Scope and Objectives of this Guide
This Guide is limited to AAC with a density of 50 lb/ft3 (800kg/m3) or less. This Guide is written for structural designers. It addresses design using factory-reinforced AAC elements. Design of AAC masonry is addressed in other documents.
Design documents produced by ACI technical committees are classified as standards ornon-standards. The latter include "guides", which are intended to present directions for analysis, design, construction, materials, or testing on a general basis. Their language is non-mandatory, permitting the user latitude in judgment concerning particular needs.
The specific objectives of this Guide are:
a) To review the basic characteristics of AAC
b) To provide a capsule history of structural applications of AAC
c) To review the fabrication of AAC elements
d) To recommend structural design procedures for factory-reinfoced AAC elements
e) To recommend construction details for use with factory-reinforced AAC elements
The structural design procedures and construction details recommended here are intended to result in AAC elements with adequate wtructural capacity, durability, appearance and overall serviceability.
B.2 TYPICAL MATERIALS AND MANUFACTURE OF AAC
B.2.1 Materials Used in AAC
Materials for AAC vary with manufacture and location, and are specified in ASTM C1386. They include some or all of the following:
a) Fine silica sand (ASTM C33, C144 or C332);
b) Class F fly ash (ASTM C 618) WITH UP TO 12% loss on ignition (LOI);
c) Hydraulic cements (ASTM C150 or C595);
d) Calcined lime (ASTM C110);
e) Gypsum (ASTM C22);
f) Expansive agent, such as finely ground aluminum powder;
g) Mixing water (clean and free of deleterious substances);
h) Reinforcement (ASTM A82), welded ro form cages, with correosion-inhibiting coating.
B.2.2 Manufacture of AAC
Overall steps in the manufacture of AAC are shown in Figure B.3.
B.2.2.1 Preparation, Batching and Mixing of Raw Materials
Sand is ground to the required fineness in a ball mill, if necessary, and is stored along with other raw materials. The raw materials are then batched by weight and delivered to the mixer. Measured amounts of water and expansive agent are added to the mixer, and the cementitious slurry is mixed.
B.2.2.2. Casting, Expansion and Initial Hydration
Steel molds are prepared to receive the fresh AAC. If reinforced AAC panels are to be produced, steel reinforcing cages are secured within the molds. After mixing, the slurry is poured into the molds. The expansive agent creates small, finely dispersed voids in the fresh mixture, which approximately triples in volume in less than an hour in the molds.
Within a few hours after casting, the initial hydration of cementitious compounds in the AAC gives it sufficient strength to hold its shape and support its own weight. The material is removed from the molds (Figure B.4) and fed into a cutting machine, which, using wires, sections the blocks and panels into the required sizes and shapes (Figure B.5). After cutting, the units remain in their original positions in the larger AAC block.
After cutting, the aerated concrete product is transported to a large autoclave, where the curing process is completed (Figure B.6). Autoclaving is required to achieve the desired structural properties and dimensional stability. The process takes about 8 - 12 hours under a pressure of about 174 psi (12 Bars) and a temperature of about 180 centigrade depending on the grade of material produced. During autoclaving, the wire-cut units remain in their original positions in the AAC block. After autoclaving, they are separated for packaging.
AAC units are normally placed on pallets for shipping. Unreinforced units are typically shrink-wrapped, while reinforced elements are banded only, using corner guards to minizmize potential localized damage that might be caused by the banding.
B.2.2.6 AAC Strength Classes
AAC is produced in different densities and corresponding compressive strengths, in accordance with ASTM C1386 (Precast Autoclaved Aerated Concrete Wall Construction Units) and ASTM C1452 (Standard Specification for Reinforced Autoclaved Aerated Concrete Elements). Densities and corresponding strengths are described in terms of "strength classes." In each case, the strength class corresponds to the specified compressive strength in MPa.
B.2.3 Typical Dimensions of AAC Units
B.2.3.1 Plain AAC Wall Units
Typical dimensions for plain AAC wall units (masonry-type units) are shown in Table B.3.
B.2.3.2 Reinforced AAC Units
Dimensional tolerances, requirements for reinforcement, and other requirements for reinforced AAC panels are specified in ASTM C1452, which also cites C1386. Typical dimensions for reinforced AAC wall units (panels) are shown in Table B.4.
B.2.4 Dimensional Tolerances
In accordance with ASTM C1386, dimensional tolerances for plain AAC wall units are 1/8 in. (3 mm) in each dimension. Dimensional tolerances for reinforced elements are given in ASTM C1452, and are listed in Table B.5.
B.2.5 Identification and Marking of AAC Units
All reinforced AAC units should bear identifying symbol to include a mark indicating the strength class, production identification code, and position number for reinforced panels. Pallets of unreinforced AAC units should be labeled with strength class, production identification code and size of units.
B.3 STRUCTURAL DESIGN OF REINFORCED AAC ELEMENTS
B.3.1 Introductory Remarks regarding Design Provisions
This document is a guide. Its design provisions are non-mandatory, and are a synthesis of design recommendations from the Autoclaved Aerated Concrete Products Association, and from the results of research conducted at the University of Alabama at Birmingham (UAB), the University of Texas at Austin (UT Austin), and elsewhere.
In this chapter, the proposed design provisions are introduced in narrative form. In appendix C (Argudo 2003), more information is presented regarding specific design provisions, and a commentary on those provisions.
The specific design provisions and their associated commentary of Appendix C (Argudo 2003), are intended to be compatible in organization, numbering and form with the design provisions of ACI 318, in order to facilitate their use by concrete designers, and also to facilitate their future consideration, in mandatory form, by ACI Committee 318. For that reason, the provisions are arranged to refer directly to ACI 318-02. Additions and exceptions are specifically noted. New subcategories are inserted for new design provisions.
Loads for structural design of AAC elements should be taken from appropriate load codes, such as ASCE 7. Understrength factors for AAC elements depend on the actions under consideration. They reflect the statistical variability of the capacity, and the accuracy of the capacity-calculation formulas. When failure is governed by yield and fracture of tensile reinforcement, factors are justifiably identical to those used for reinforced concrete. When failure is governed by crushing or diagonal tension of the AAC itself, factors are similar to those used for concrete. They may even be higher, because the factory production of AAC leads to decreased variability in its mechanical characteristics compared to conventional concrete.
The design provisions of this Guide are not intended for use with unreinforced, masonry-type units. Design of those units is covered by provisions currently under development within the Masonry Standards Joint Committee.
B.3.2 Proposed Design Provisions for Reinforced AAC Panels
B.3.2.1 Basic Design Assumptions
The proposed design provisions for reinforced AAC panels are based on the same principles used for strength design of conventional reinforced concrete elements: strain compatibility between AAC and reinforcement (with some modifications as noted below); stress-strain behavior of AAC and reinforcement; and equilibrium. The design strength of AAC in compression is based on a specified design compressive strength is verified by compressive strength testing, using ASTM C1386, when the AAC panels are fabricated. The design strength of AAC in tension is proposed as a function of the specified compressive strength. The design strength of reinforcement in tension is proposed as the specified yield strength.
B.3.2.2 Combinations of Flexure and Axial Load
AAC panels are designed for combinations of flexural and axial load using principles identical to those for conventional reinforcement. Nomianl capacity is computed assuming plane section; tensile reinforcement is assumed to be yielded; the stress in compressive reinforcement is computed based on its strain and its stress-strain behavior; and the distribution of compressive stress in the AAC is approximated by an equivalent rectangular stress block.
Because reinforced AAC panels usually have equal areas of tensile and compressive reinforcement, flexural capacity is usually "tension-controlled" (in the terminology of ACI 318-02. Section are under-reinforced (in the terminology of ACI 318-99).
B.3.2.3 Bond and Development of Reinforcement
Reinforcement in AAC panels consists of welded-wire mesh installed when the panels are produced, and deformed reinforcement installed in 3- to 4- in. grouted cores as the panels are erected.
Bond and development requirements for deformed reinforcement in grout are identical to those used for concrete or masonry construction. Given the small sizes of deformed bars used in AAC construction, bond between the grout and the AAC itself does not govern the bond capacity.
Bond and development requirements for welded-wire fabric embedded in AAC are quite different from those for conventional concrete, however. Because the welded-wire fabric has a corrosion-resistant coating, bond strength between the coated wire and the AAC itself is negligible. Bond strength comes from bearing of the cross wires against the AAC. For typical cross-wire spacings, local crushing of the AAC under the cross wires can be assumed to redistribute the bearing stresses under the cross wires, leading to a uniform bearing strength of AAC' under every corss-wire. Muptiplying this stress by the number of cross wires and by the bearing are of each cross-wire gives the maximum force that can be developed in the welded wire fabric (Figure B.8).
This maximum force in the welded-wire mesh can limit the flexural capacity of a reinforced AAC panel.
As with conventional reinforced concrete elements, the shear resistance of AAC elements is computed as the summation of a shear resistance due to the AAC itself (Vaac), and a shear resistance due to reinforcement oriented parappel to the direction of the shear.
The shear resistance due to the AAC itself (Vaac) is computed using the web-shear approach of ACI 318-02. The diagonal tension resistance of the AAC is expressed in terms of its specified compressive strength, and principal tensile stresses, including the effects of axial loads, are equated with this strength. This produces an expression for Vaac in terms of the diagonal tension resistance of the AAC, and the axial load on the element.
The shear resistance due to transverse reinforcement is computed based on the cross-sectional area of the transverse reinforcement crossing a hypothetical 45-degree crack in the AAC. As explained in the previous subsection, it may also be limited by bond and development of the reinforcement.
To prevent local crushing of the AAC, nominal stresses in it are limited to fAAC'. When AAC floor or roof panels bear on AAC walls, shear failure of the edge of the wall is also possible. This is handled by limiting the shear stress on potential inclined failure surfaces.
B.4 HANDLING, EXECTION AND CONSTRUCTION WITH AAC UNITS
B.4.1 Handling of AAC Panels
AAC panels should be stored on suitably prepared supports, so that they are prevented from warping. They should be carefully placed in their final position without being overstressed or damaged. Instructions from the manufacturer on how to handle the units should be followed. Special equipment is usually used or recommended by the manufacturer to assist in the transportation and erection of the units.
B.4.2 Erection of AAC Wall Systems
AAC panels are lifted and placed using specially designed clamps, and are alingned using alignment bars.
B.4.2.1 Erection of AAC Cladding Systems
AAC panels can be used as non-load bearing cladding systems. This application usually involves horizontally oriented panels attached to steel or reinforced concrete frame. Erection of such panels follows these steps:
a) Ensure that supporting columns are plumb and true.
b) Set the bottom panel against the supporting columns and over the floor slab or slab on ground, on top of a bed joint of conventional masonry mortar. Make sure that the panel is true and level.
c) Immediately after placing the first panel, fasten a wall anchor plate to the column (uing a dovetail or mechanically locking connector0, and nail the plate to the AAC panel. The back face of the panel should be flush with the outer face of the column.
d) Place subsequent panels on top of the first one. The top and bottom faces of the horizontal wall panels can have eithera tongue and groove profile, or a flat profile. Tongue and groove joints do not require mortar. Flat joints are mortared with thin-bed mortar.
e) Seal horizontal and vertical joints with flexible sealant.
B.4.2.2 Erection of Vertical AAC Panels for Bearing-Wall Systems
Vertical AAC panels may also be used as a load-bearing wall system. In such cases, the floor roof systems are usually designed and detailed as horizontal diaphragms to transfer lateral loads to shear walls. The tops of the panels are connected to the floor or roof diaphragms using a cast-in-place reinforced concrete ring beam. This and many other structural details are addressed in the next chapter.
When vertical wall panels are used in this way, they are set on a bedding joint of conventional masonry mortar, with or without a waterproofing admixture. Vertical wall panels are usually mortared together with thin-bed mortar.
B.4.3 Erection of AAC Floor and Roof Panels
AAC floor and floor panels can be erected on concrete, steel or masonry construction. All bearing surfaces should be level and minimum required bearing areas (to prevent local crushing) should be maintained.
As in any precast construction system, care must be exercised in the installation of the first panel to ensure correct alignment of the remaining panels. All floor and roof anchors should be installed prior to placement of the panels, thus streamlining and expediting panel installation.
Most floor and roof panels are connected by keyed joints that are reinforced and filled with grout to lock the panels together and provide diaphragm action to resist lateral loads. A cast-in-place reinforced concrete ring beam is normally placed along the perimeter of the diaphragm, completing the system.
B.4.4 Electrical and Plumbing Installations in AAC
Electrical and plumbing installations in AAC are placed in routed chases. Care should be taken when laying out chases to ensure that the structural integrity of the AAC elements is maintained. Do not cut reinforcing steel or reduce the structural thickness of the AAC elements in critical areas. When analyzing the AAC element is intended to span vertically, horizontal routing should be permitted only in areas with low flexural and compressive stresses. In contrast, when the AAC element is intended to span horizontally, vertical routing should be minimized. When possible, it may be advantageous to provide designated chases for large quantities of conduit or plumbing.
B.4.5 Exterior Finishes for AAC
Unprotected exterior AAC deteriorates when exposed to cycles of freezing and thawing while saturated. To prevent such freeze-thaw deterioration, and to enhance the aesthetics and abrasion resistance of AAC, exterior finishes should be used. They should be compatible with the underlying AAC in terms of thermal expansion and modulus of elasticity, and should be vapor permeable. Many different types of exterior finishes are available, and the most common are discussed here.
B.4.5.1 Polymer-Modified Stuccos, Paints or Finish Systems
Polymer-modified stuccos, paints or finish systems are the most common exterior finish for AAC. They increase the AAC's water-penetration resistance while allowing the passage of water vapro. Heavy acrylic-based paints containing aggregates are also used to increase abrasion resistance. There is generally no need to level the surface, and horizontal and vertical joints may be chamfered as an architectural feature, or may be filled.
B.4.5.2 Masonry Veneer
Masonry veneer may be used over AAC panels in much the same way that it is used over other materials. The veneer is attached to the AAC wall using masonry ties. The space between the AAC and the masonry can be left open (forming a drainage wall), or can be filled with mortar.
B.4.5.3 Finishes for Basement Walls
When AAC panels are used in contact with moist or saturated soil (for example, in basement walls, the surface in contact with the soil should be coated with a waterproof material or membrance. The interior surface should either remain uncoated, or be coated with a vapor-permeable interior finish.
B.4.6 Interior Finishes for AAC Panels
Interior finishes are used to enhance the aesthetics and durability of AAC. They should be compatible with the underlying AAC in terms of thermal expansion and modulus of elasticity, and should be vapor permeable. Many different types of interior finishes are available, and the most common are discussed here.
B.4.6.1 Interior Plasters
Interior AAC wall panels may have a thin coat of a mineral-based plaster to achieve a smooth finished surface. Lightweight interior gypsum-based plaster may provide a thicker coating to level and straingten walls, and to provide a base for decorative interior paints or wall finishes. Interior plasters have bonding agents to enhance their adhesion and flexibility, and are commonly installed by either spraying or troweling.
B.4.6.2 Gypsum Board
When applied to the interior surface of exterior AAC walls, gypsum board should be attached using pressure-treated furring strips. When applied to interior walls, moisture-resistant gypsum board can be applied directly to the AAC surface.
B.4.6.3 High-Durability Finishes for Commercial Applications
For commercial applications requiring high durability and low maintenance, acrylic-based coatings are often used. Some contain aggregates to enhance abrasion resistance.
B.4.6.4 Cearmic Tile
When ceramic wall tile is to be applied over AAC, surface perparation is normally necessary only when the AAC surface requires leveling. In such cases, a Portland cement- or gypsum-based parge coat is applied to the AAC surface before setting the ceramic tile. The ceramic tile should then be adhered to the parged wall using either a cement-based thin-set mortar or an organic adhesive. In moist areas such as shower, only a Portland cement-based parge coat should be used, and the ceramic tile should be set with cement-based thin-set mortar only.