Wind-Tunnel Investigation of Effect of Yaw on Lateral-Stability Characteristics V-Symmetrically Tapered Wing with Circular Fuselage Having Horizontal and Vertical Tail. (Advance Restricted Report 3F23 June 1943)
Wind-tunnel investigation of effect of yaw on lateral-stability characteristics V-symmetrically tapered wing with circular fuselage having horizontal and vertical tail
Nat Advisory Committee Aeronautics -- Wartime Report
1943
15 pages
13 Supp plates
Report
Englisch
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