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Aerodynamic characteristics in pitch of several triple-body missile configurations at Mach numbers 0.6 to 1.4
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 (2)
Subject
Charts, diagrams, etc (2) *
Airplanes--Models--Testing (1)
Airplanes--Models--Wings (1)
Airplanes--Wings, Swept-back (1)
Cone--Aerodynamics (1)
Cylinders--Aerodynamics (1)
Drag (Aerodynamics) (1)
Flaps (Airplanes) (1)
Leading edges (Aerodynamics) (1)
Lift (Aerodynamics) (1)
Pitching (Aerodynamics) (1)
Rockets (Aeronautics) (1)
Stability of airplanes, Longitudinal (1)
Author
Knechtel, Earl D. (2) *
Andrea, Arvid N. (1)
Lee, George. (1)