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Aerodynamic investigation at Mach number 1.92 of a rectangular wing and tail and body configuration and Its components

Aerodynamic characteristics of a leading-edge slat on a 35 degree swept-back wing for Mach numbers from 0.30 to 0.88

Aerodynamic characteristics in pitch of several triple-body missile configurations at Mach numbers 0.6 to 1.4

Experimental determination of damping in pitch of swept and delta wings at supersonic Mach numbers

Investigation of the aerodynamic characteristics in pitch and sideslip of a 45©� swept-wing airplane configuration with various vertical locations of the wing and horizontal tail.Static lateral and directional stability; Mach numbers of 1.41 and 2.01

Recent design studies directed towards elimination of pitch-up

Published Year

• 1950-1959 (6) *

Subject

• Pitching (Aerodynamics) (6) *
• Charts, diagrams, etc (5)
• Airplanes--Wings, Swept-back (3)
• Drag (Aerodynamics) (3)
• Lift (Aerodynamics) (3)
• Wind tunnel testing (3)
• Airplanes--Tail surfaces (2)
• Aerodynamic load (1)
• Aerodynamics, Supersonic (1)
• Airplanes--Design and construction (1)
• Airplanes--Models--Testing (1)
• Airplanes--Wings, Rectangular (1)
• Airplanes--Wings, Triangular (1)
• Airplanes--Wings--Testing (1)
• Cone--Aerodynamics (1)
• Cylinders--Aerodynamics (1)
• Mach number (1)
• Rockets (Aeronautics) (1)
• Stability of airplanes, Lateral (1)

Author

• Andrea, Arvid N. (1)
• Ellis, Macon C. (1)
• Gray, W. H. (1)
• Grigsby, Carl E. (1)
• Hayter, Nora-Lee F. (1)
• Kelly, John A. (1)
• Knechtel, Earl D. (1)
• Moore, John A. (1)
• Robinson, Ross B. (1)
• Spearman, M. Leroy. (1)
• Weil, Joseph. (1)

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