Stability and Control Characteristics at Low Speed of Airplane Model Having 38.7° Sweptback Wing with Aspect Ratio 4.51, Taper Ratio 0.54, and Conventional Tail Surfaces.
Stability and control characteristics at low speed of airplane model having 38.7° sweptback wing with aspect ratio 4.51, taper ratio 0.54, and conventional tail surfaces
Nat Advisory Committee Aeronautics -- Tech Note
1948
155 pages
Report
Englisch
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