Considers cantilever wing with two spars and similar wing with three spars in approximate computation; author seeks to determine effect of variously loaded spars on one another, since neglect of this effect would present economically very unfavorable computation method.
Computation of cantilever airplane wings
U.S. Nat. Advisory Comm. Aeronautics -- Tech. Memorandums
1925
21 pages
15 Figs. on supp. plates
Report
Englisch
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Computation of cantilever airplane wings
NTRS | 1925
|NTRS | 1989
Engineering Index Backfile | 1921
Engineering Index Backfile | 1935
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