Sheet in airplane wings, fuselages, and hull bottoms reinforced by stringers frequently is subjected to normal pressure as well as forces in plane of sheet; solution presented for buckling load and load carried after buckling of clamped plate having width-length ratio of 1:4 under combined normal pressure and axial load. See also Engineering Index 1945 p 844.
Clamped long rectangular plate under combined axial load and normal pressure
Nat Advisory Committee Aeronautics -- Tech Note
1946
14 pages
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English
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