The stress distribution in shell bodies and wings as an equilibrium problem (1937)
NASA Technical Reports Server (NTRS) · leaf 26
F.A.C.A. Technical Memorandum Ho. 817 7128.11,12,13 … 5 Figure 12.- Stress In end bulkhead due to applied transverse load. Figure 13.- Improved end bulkhead design.
NASA Technical Reports Server (NTRS)
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