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The analysis of non-linear dynamic behavior (including snap-through) of postbuckled plates by simple analytical solutionStatic postbuckling and nonlinear dynamic analysis of plates are usually accomplished by multimode analyses, although the methods are complicated and do not give straightforward understanding of the nonlinear behavior. Assuming single-mode transverse displacement, a simple formula is derived for the transverse load displacement relationship of a plate under in-plane compression. The formula is used to derive a simple analytical expression for the static postbuckling displacement and nonlinear dynamic responses of postbuckled plates under sinusoidal or random excitation. Regions with softening and hardening spring behavior are identified. Also, the highly nonlinear motion of snap-through and its effects on the overall dynamic response can be easily interpreted using the single-mode formula. Theoretical results are compared with experimental results obtained using a buckled aluminum panel, using discrete frequency and broadband point excitation. Some important effects of the snap-through motion on the dynamic response of the postbuckled plates are found.
Document ID
19880013055
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ng, C. F.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1988
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-89165
NAS 1.15:89165
Accession Number
88N22439
Funding Number(s)
PROJECT: RTOP 505-63-11-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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