Report on test with two biplanes differing greatly in wing-cellule arrangement; effects of spinning characteristics of varying center-ofgravity location, mass distribution, control position and engine power; rearward weight added behind wings delays recovery from spin. (See also Soc. Automotive Engrs. -- Jl vol. 27, no. 5, Nov. 1930 pp. 573-577, 3 figs)
Airplane tail-spins analyzed
Aircraft Eng
Aircraft Engineering ; 2 , n 21
1930
3 pages
2 Figs.
Article (Journal)
English
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Engineering Index Backfile | 1930
|Engineering Index Backfile | 1927
|Engineering Index Backfile | 1929
|Engineering Index Backfile | 1929
|SAE Technical Papers | 1929
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