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 Aircraft Eng., vol. 2, no. 21, Nov. 1930, pp. 284-286, 2 figs)
Airplane tail-spins analyzed
Soc. Automotive Engrs. -- Jl
Society of Automotive Engineers -- Journal ; 27 , n 5
1930
5 pages
3 Figs.
Article (Journal)
English
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Engineering Index Backfile | 1930
|Engineering Index Backfile | 1929
|SAE Technical Papers | 1929
|Engineering Index Backfile | 1929
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