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Load Tests on a Stiffened Circular Cylindrical Shell (1938)
NASA Technical Reports Server (NTRS) · leaf 31
Fig. 22 N.A.C.A. Technical Memorandum No. 864 Strips >r r- c /?' 1 A' TP 36 n7fct rp IP The peripheral stresses in the strips A B C D are obtained lay reflection of the curves A'B'C1©1 … TP Cross section IP srp / V it r, x 7=m Cylinder perimeter \ \ 15 18 10 11 12 13 It 17 16 Longitudinal stiffener.NASA Technical Reports Server (NTRS)
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