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Application of aeroelastic constraints in structural optimizationAircraft structural weight optimization for given fundamental vibration frequency obtained by applying aeroelastic constraints, using analytical approach
Document ID
19700038115
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ashley, H.
Mcintosh, S. C., Jr.
Date Acquired
August 5, 2013
Publication Date
January 1, 1969
Publication Information
Publisher: SPRINGER- VERLAG,
Subject Category
Structural Mechanics
Meeting Information
Meeting: APPLIED MECHANICS, INTERNATIONAL UNION OF THEORETICAL AND APPLIED MECHANICS, INTERNATIONAL CONGRESS, 12TH, STANFORD U.
Location: STANFORD, CA
Start Date: August 26, 1968
End Date: August 31, 1968
Sponsors: APPLIED MECHANICS
Accession Number
70A14231
Funding Number(s)
CONTRACT_GRANT: NGR-05-020-102
CONTRACT_GRANT: AF 44/620/-68-C-0036
Distribution Limits
Public
Copyright
Other

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