Empirical method presented; general method of summing crippling loads of component elements of stiffener and then dividing by summation of elemental areas to obtain crippling stress, is discussed in several texts; however, enough test data have not been available heretofore to establish general empirical curves for predicting strength of any stiffener or stiffened panel of reasonable proportions.
Predicting stiffener and stiffened panel crippling stresses
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 9 , n 13
1942
9 pages
Article (Journal)
English
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