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RR 22.10.00-3.3 Chinese Response Spectrum Enhancements

Reponse spectra per the GB50011 2010 code may now consider torsional effects of the load.

Inherent and Accidental Torsion

Note: STAAD.Pro does not support the coupled torsion methodology as per GB50011-2010. This implementation enables the general "inherent and accidental torsion" for GB50011 response spectrum analysis. Note that this implementation does not comply with Cl. 5.2.3 of GB50011-2010.

In response spectrum analysis all the response quantities (i.e., joint displacements, member forces, support reactions, plate stresses, etc.) are calculated for each mode of vibration considered in the analysis. These response quantities from each mode are combined using a modal combination method (either CQC or SRSS) to produce a single positive result for the given direction of acceleration. This computed result represents a maximum magnitude of the response quantity that is likely to occur during seismic loading. The actual response is expected to vary from a range of negative to the positive value of this maximum computed quantity.

No information is available from response spectrum analysis as to when this maximum value occurs during the seismic loading and what will be the value of other response quantities at that time. For example, consider two joints J2 and J3 whose maximum joint displacement in the global X direction come out to be X1 and X2 respectively. This implies that during seismic loading joint J1 will have X-direction displacement that is expected to vary from -X1 to +X1 and that for joint J2 from -X2 to +X2. However, this does not necessarily mean that the point of time at which the X displacement of joint J1 is X1, the X displacement of joint J2 will also be X2.

For the reason stated above, the torsional moment at each floor arising due to dynamic eccentricity along with accidental eccentricity (if any) is calculated for each mode. Lateral story shear from this torsion is calculated forming global load vectors for each mode. Static analysis is carried out with this global load vector to produce global joint displacement vectors for each mode due to torsion. These joint displacements from torsion for each mode are algebraically added to the global joint displacement vectors from response spectrum analysis for each mode. The final joint displacements from the response spectrum along with torsion for all modes are combined using a specified modal combination method to get the final maximum possible joint displacements.