Experimental and analytical investigation of a monocoque wing model loaded in bending (1939)
NASA Technical Reports Server (NTRS) · leaf 38
l Memorandum So. 915 Jigs* 9,10,11,12,13 Stresses according to *J Stresses according to plementary bending theory K elementary bending theory f Measured 5? 5 Figure 9.- Longitudinal stresses in Figure 10.- Longitudinal stresses in the case of pure bending the case of pure bending by couples at the… … Flange Figure 11.- Effect of buckling L of the skin on the stress distribution in the Panel case of bending transverse Figure 13.- Designation of the loads at the free ends of the webs. panel* in the. akin.
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