Experimental work done by National Advisory Committee for Aeronautics on panels; resulting design charts developed for 24S-T aluminum alloy panels with formed Z section stiffeners and for 24S-T and 75S-T aluminum alloy panels with extruded Y-section stiffeners. (See also - discussion p 143-4)
Design charts for longitudinally stiffened wing compression panels
Soc Automotive Engrs -- Trans
1949
21 pages
Article (Journal)
English
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DESIGN CHARTS for Longitudinally Stiffened Wing Compression Panels
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