Table computed for hypothetical material having stress values of fb., ft., and fs. equal to 10 tons per sq. in.; it is arranged such that for any given material fb., fs., and ft. values within limits enumerated may be obtained by simple proportion of required and hypothetical stress values. (Aircraft Eng.)
Detail stressing
Flight
Flight ; 21 , n 5
1929
2 pages
Table
Article (Journal)
English
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