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Analysis of nonlinear panel flutter and response under random excitation or nonlinear aerodynamic loadingNonlinear panel flutter analysis and response under random excitation or nonlinear aerodynamic loading, using Rayleigh-Ritz approximation to Hamilton variational principle
Document ID
19710041383
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Eastep, F. E.
Mcintosh, S. C., Jr.
Date Acquired
August 6, 2013
Publication Date
March 1, 1971
Subject Category
Structural Mechanics
Accession Number
71A22080
Funding Number(s)
CONTRACT_GRANT: NGR-05-020-102
Distribution Limits
Public
Copyright
Other

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