Curves obtained show total increase in weight of optimum designed sheet stiffener compression panel when skin thickness is increased by arbitrary amount; curves are based on data from tests conducted by NACA on 75S-T Y-stiffened panels; method may also be applied to plotting of other sheet stiffener compression panel data.
Effect of torsional stiffness requirements on wing structural weight
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 17 , n 11
1950
5 pages
Article (Journal)
English
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