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NASTRAN nonlinear vibration analysis of beam and frame structuresA capability for the nonlinear vibration analysis of beam and frame structures suitable for use with NASTRAN level 15.5 is described. The nonlinearity considered is due to the presence of axial loads induced by longitudinal end restraints and lateral displacements that are large compared to the beam height. A brief discussion is included of the mathematical analysis and the geometrical stiffness matrix for a prismatic beam (BAR) element. Also included are a brief discussion of the equivalent linearization iterative process used to determine the nonlinear frequency, the required modifications to subroutines DBAR and XMPLBD of the NASTRAN code, and the appropriate vibration capability, four example problems are presented. Comparisons with existing experimental and analytical results show that excellent accuracy is achieved with NASTRAN in all cases.
Document ID
19750023427
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mei, C.
(LTV Aerospace Corp. Hampton, VA, United States)
Rogers, J. L., Jr.
(NASA Langley Research Center)
Date Acquired
August 8, 2013
Publication Date
September 1, 1975
Publication Information
Publication: NASTRAN: Users' Experiences
Subject Category
Structural Mechanics
Accession Number
75N31500
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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