With reference to aircraft practice, formula for buckling under compression of flat rectangular plate stiffened only transversely is applied to design problem of determining least total weight of material necessary to support specified load; successive steps in process described with least possible reference to mathematical analysis. (See also - discussion pt 8 July/Aug p D175-8)
Design of transversely stiffened flat plating
North-East Coast Instn Engrs Shipbldrs -- Trans
1950
14 pages
Aufsatz (Zeitschrift)
Englisch
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Minimum-weight design of simply supported transversely stiffened plates under compression
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