Investigation to study spin behavior of fighter type aircraft, carried out in Chance Vought low speed wind tunnel: exploratory one degree of freedom tests; 2-dimensional tests; determination of autorotation moments of complete model; it is revealed that fuselage nose, rather than wing, is major source of autorotative moment; other factors influencing spin behavior.
Autorotation of fuselages
Aeronautical Eng Rev
Aeronautical Engineering Review ; 17 , n 2
1958
4 pages
Article (Journal)
English
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