Experimental and analytical investigation of a monocoque wing model loaded in bending (1939)
NASA Technical Reports Server (NTRS) · leaf 39
V.A.C.A. Technical Memorandum Vo. 915 Tig*. 14,15 Figure 14.-* Shear flow in the case of bending py concentrated loads at free ends of the webs (total transverse load, Q = 1700 kg [3760 lb.] heavy curve: shear flow determined from the strain measure- ments. Light horisontal lines: calculated… … Figure 15.- Shear flow in the case of bending by uniformly distributed transverse loads on the webs. Total transverse load Q= 1700 kg [3760 lb.] heavy curve: shear flow determined from the strain measurements. Light horisontal lines: calculated values.
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