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Experimental and analytical investigation of a monocoque wing model loaded in bending (1939)

NASA Technical Reports Server (NTRS) · leaf 37

An illustration from Experimental and analytical investigation of a monocoque wing model loaded in bending, 1939, leaf 37
H.A.C.A. Technical Memorandum Ho. 915 4.6,7.8 Restraint _L**d- Figure 4.- Test set tip. ft! JSiJJ** ^ co**en\r*ted transverse forces at the ends of the web. b Bending by uniformly distributed transverse forces on the webs (c) Pure bending by couples at the spar chords (d) Pure bending tqr a couple… … Figure 7— Longitudinal stresses Figure 8.- Longitudinal stresses in the case of bending in the case of bending with a concentrated transverse by uniformly distributed loads on force at the ends of the webs the webs (Figure 6b, total trans- (Figure 6av total transverse load verse load $ s 1700 kg…

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