Experimental and theoretical evidence drawn upon to show that, due to shear lag, airplane wing with longitudinal stringers should be less efficient from strength weight standpoint than wing which does not have longitudinal stringers in addition to main wing beams.
Effect of shear lag upon wing strength
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 6 , n 10 ; p 418-420
1939
3 pages
Bibliography
Article (Journal)
English
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