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Minimum weight design with structural reliability
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Minimum weight design with structural reliability
Minimum weight design with structural reliability
HS
Harold Switzky
Harold Switzky
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1 May 1965
journal article
Published by
American Institute of Aeronautics and Astronautics (AIAA)
in
Journal of Aircraft
Vol. 2
(3)
,
228-232
https://doi.org/10.2514/3.43644
Abstract
No abstract available
Keywords
STRUCTURAL RELIABILITY
MINIMUM WEIGHT DESIGN
DESIGN WITH STRUCTURAL
Cited by 7 articles