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On the Strength of Box Type Fuselages (1929)
NASA Technical Reports Server (NTRS) · leaf 12
• C.A. Technical tleiaorandwi No.511 Figs.1,3,11,12. s Deformation of the tested cay for F ■ 200 kg (661.39 11.) 12.1 6 6 A 5NASA Technical Reports Server (NTRS)
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