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h2. How do I obtain collector forces within a floor diaphragm? *Answer:* The collector forces within a floor diaphragm may be measured through the following process: \\ \\ # Define a semi-rigid diaphragm, then apply diaphragm forces, as shown in Figure 1: \\ \\ \\ !worddav6c318e212bb3a785ed1e6ac7e3308523.png|align=center,border=0!\\ {center-text}Figure 1 - Apply diaphragm forces{center-text} \\ \\ \\ # For a given [load case|kb:Load case], display any stress or [shell|kb:Shell] force, as shown in Figure 2: \\ \\ \\ !worddavd26cf2b3a7f5b7dfb2c859960d4042b5.png|align=center,border=0!\\ {center-text}Figure 2 - Display stress or shell force{center-text} \\ \\ \\ # Where maximum chord forces are expected, draw or define a section cut, as shown in Figure 3: \\ \\ \\ !worddavb9bce433f4a6f0d8da6c5b32e1a93d47.png|align=center,border=0!\\ {center-text}Figure 3 - Maximum chord forces{center-text} \\ \\ \\ # Moments about the Z-axis represent in-plane moments. Ensure that the resultant-force angle is 90 in order to enforce vertical line, then select Refresh, as shown in Figure 4: \\ \\ !2013-03-07_1427worddav2c11c3f891465985ec44e2e13afd6298.png|border=1,align=center!\\ \\ {center-text}Figure 4 - In-plane moment{center-text} \\ \\ \\ # Compression and tension chord forces are then given as the value of each Z-axis moment divided by slab width, as shown in Figure 5: \\ \\ \\ !worddav9f256fcb1daf7bef870b821873738f90.png|align=center,border=0!\\ {center-text}Figure 5 - Compression and tension chord forces{center-text} \\ \\ \\ # For shear and collector forces located at the connection between the diaphragm and a shear wall, draw or define a section cut next to the support which follows the wall direction, as shown in Figure 6: \\ \\ \\ !worddav2be42fafeaac037a13a3e192ae5b9bc2.png|align=center,border=0!\\ {center-text}Figure 6 - Shear and collector forces{center-text} \\ \\ \\ # Again, ensure that the resultant-force angle is 90, and refresh as necessary. Given this example model, the shear/collector force, which is presented in F1, is 2559 lbs., as shown in Figure 7: \\ \\ \\ !2013-03-07_1421.png|border=1,align=center!\\ {center-text}Figure 7 - Shear and collector forces {center-text} # Local axis of section cut 1, 2 and Z are similar to a frame element, resultant force angle indicates angle between X global axis and section cut local 1 axis \\ h1. See Also * [Rigid vs. semi-rigid diaphragm|Rigid vs. Semi-rigid diaphragm] article * [etabs:Accidental eccentricity design] article |
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