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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

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) *

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