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Metal Covering of Airplanes (1930)
NASA Technical Reports Server (NTRS) · leaf 20
Fig.19 N.A.C.A. Technical Momorandun No.592 Loading: P = 60 kg Seals of displacement 8 16x10 °cm 0 0 40 100 fcg/cm2 Scale of stress Compression strut … Fig.19 Stresses and displacements in examiner beam panel a,b,c, & d (Fig.ll).NASA Technical Reports Server (NTRS)
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