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Effects of wing-tip droop on the longitudinal characteristics of two highly swept wing-body combinations at Mach numbers from 0.6 to 1.4
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Published Year
1950-1959 (1)
Subject
Airplanes--Models--Testing (1)
Airplanes--Models--Wings (1) *
Airplanes--Wings, Swept-back (1)
Charts, diagrams, etc (1)
Flaps (Airplanes) (1)
Leading edges (Aerodynamics) (1)
Stability of airplanes, Longitudinal (1)
Author
Knechtel, Earl D. (1) *
Lee, George. (1)
