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Structural optimization with flutter speed constraints using maximized step sizeA procedure is presented for the minimization of structural mass while satisfying flutter speed constraints. The procedure differs from other optimization methods in that the flutter speed is exactly satisfied at each resizing step, and the step size is determined by a direct minimization of the objective function (mass) for each set of flutter derivatives calculated. In conjunction with this method, a new move vector is suggested which results in a very efficient resizing procedure.
Document ID
19750048593
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Oconnell, R. F.
Radovcich, N. A.
Hassig, H. J.
(Lockheed-California Co. Burbank, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
May 1, 1975
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 75-778
Accession Number
75A32665
Funding Number(s)
CONTRACT_GRANT: NAS1-12121
Distribution Limits
Public
Copyright
Other

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