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Differential stiffness effectsDifferential stiffness as developed in NASTRAN is a linear change in stiffness caused by applied loads. Examples of differential stiffness are the stiffening effects of gravity forces in a pendulum, centrifugal forces in rotor blades and pressure loading of shell structures. In cases wherein this stiffness caused by a load is destabilizing, the differential stiffness concept lends itself to nonlinear structural analysis. Rigid Formats 4 (static analysis with differential stiffness) and 13 (normal modes with differential stiffness) are specifically designed to account for such stiffness changes. How pressure loading may be treated in these rigid formats is clarified. This clarification results from modal correlation of Ground Vibration Test (GVT) results from the empty and pressurized Filament Wound Case (FWC) quarter-scale Space Shuttle solid rocket booster (QSSRB). A sketch of the QSSRB cantilevered to the floor by its external tank attachments is shown.
Document ID
19860016361
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ujihara, B. H.
(Rockwell International Corp. Pittsburgh, PA, United States)
Tong, E. T.
(Rockwell International Corp. Pittsburgh, PA, United States)
Date Acquired
August 12, 2013
Publication Date
May 1, 1986
Publication Information
Publication: COSMIC 14th NASTRAN (R) Users' Colloquium
Subject Category
Structural Mechanics
Accession Number
86N25833
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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