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
01.07.1925
Sonstige
Keine Angabe
Englisch
Computation of cantilever airplane wings
Engineering Index Backfile | 1925
|Engineering Index Backfile | 1921
NTRS | 1989
Engineering Index Backfile | 1935
|