Tests made on model of airplane with zero stagger, fairly small gap-chord ratio, and round-section fuselage; and wind-channel tests of pitching and yawing moments with sideslip made with a view to finding any reasons why it should be difficult to bring airplane of this type out of a spin.
Pitching and yawing moments with sideslip on a model aeroplane with zero stagger
Aeronautical Research Committee -- Reports Memoranda
1925
14 pages
15 Figs. on supp. plates
Article (Journal)
English
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Effects of sideslip on rolling and yawing moments
TIBKAT | 1932
|Effects of sideslip on rolling and yawing moments
SLUB | 1932
|