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ON THE EFFECTS OF CIRCULAR BOLT PATTERNS ON THE ...

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The instrumented bolts were connected to the data acquisition system and the shunt of the Wetson-<br />

Bridge was zeroed and calibrated while the bolts were in a relaxed state. The LVDTs and load cell were<br />

connected to the data acquisition system and all the readings were set to zero. The bolts were then<br />

tightened, using a calibrated torque-wrench to the proof load specified by the LRFD design manual [1]. A<br />

cross-pattern tightening sequence was used. The bolts were pre-tensioned in two steps to prevent the<br />

damage to the bolts and the instrumentation. The two pieces of the T-Stubs were pulled together in the<br />

first step of bolt tightening, and the proof load was applied on the second step.<br />

A monotonic load was applied on to the specimen at approximately5kips/min. The specimens were<br />

loaded to failure. The observations were documented and the photographs were taken while the test was<br />

in progress.<br />

3.2.6 Test Results<br />

As mentioned before, the main scope of this experimental study was to investigate the behavior of<br />

the T-Stubs under various bolt pattern configuration. In addition, the data collected in this section was<br />

used to validate the results of the numerical models in Chapter-4.<br />

Table 3-2 shows the summary of the test results. The tensile yield forces presented in this table are<br />

determined by using a bi-linear curve fit of the T-Stubs data. In addition, the flange separations versus<br />

the applied force for three specimens are presented and compared in Figure 3-14. The first line<br />

represents the initial stiffness of the T-Stubs and the second line represents the post-yield stiffness. The<br />

intersection of the two lines is considered as the yielding tensile force; thus, the corresponding flange<br />

separation is recorded as flange separation at yield (∆y). The ultimate tensile force (Pu) is the maximum<br />

tensile force resisted by the specimen, and the maximum flange separation was reported as ∆u in this<br />

table.<br />

34

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