The purpose of this treatise is, first of all, the determination of the effect of variously loaded spars on one another, since the neglect of this effect would present an economically very unfavorable computation method. The system of spars and cross-bars alone (whether solid or built-up) does not matter at first, the original assumption being that the spars are rigidly braced by the cross-bars.
Computation of cantilever airplane wings
1925-07-01
Miscellaneous
No indication
English
Computation of cantilever airplane wings
Engineering Index Backfile | 1925
|NTRS | 1989
Engineering Index Backfile | 1921
Engineering Index Backfile | 1935
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