Study relating to missile components with particular reference to plates having aspect ratios a/b for values equal to or greater than 1 or equal to or less than 4.
Critical buckling stresses of simply supported flat rectangular plates under combined longitudinal compression, transverse compression, and shear
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 21 , n 6
1954
6 pages
Aufsatz (Zeitschrift)
Englisch
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