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The analysis of nonlinear panel flutter and response under random excitation or nonlinear aerodynamic loadingNonlinear panel flutter for random excitation and linear/nonlinear aerodynamic loading, using Rayleigh-Ritz approximation to Hamilton variational principle
Document ID
19700050989
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Eastep, F. E.
Mcintosh, S. C., Jr.
Date Acquired
August 5, 2013
Publication Date
January 1, 1970
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, INC.,
Subject Category
Structural Mechanics
Meeting Information
Meeting: MATERIALS AND STRUCTURAL DYNAMICS, AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS AND AMERICAN SOCIETY OF MECHANICAL ENGINEERS, STRUCTURES, STRUCTURAL DYNAMICS, AND MATERIALS CONFERENCE, 11TH
Location: DENVER, CO
Start Date: April 22, 1970
End Date: April 24, 1970
Sponsors: MATERIALS AND STRUCTURAL DYNAMICS
Accession Number
70A27105
Funding Number(s)
CONTRACT_GRANT: NGR-05-020-102
Distribution Limits
Public
Copyright
Other

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