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Normal force, center of pressure, and zero-lift drag of several ballistic-type missiles at Mach numbers of 4.05

Experimental aerodynamic forces and moments at low speed of a missile model during simulated launching from the midsemispan location of a 45 degree sweptback wing-fuselage combination

Stability of two rocket-propelled models having aspect-ratio-5 unswept tails on a long body for the Mach number range of 1.7 to 2.4

Published Year

• 1950-1959 (3) *

Subject

• Charts, diagrams, etc (3)
• Rockets (Aeronautics)--Models (3) *
• Aerodynamics (1)
• Aerodynamics, Supersonic (1)
• Airplanes--Wings, Swept-back (1)
• Aspect ratio (Aerofoils) (1)
• Ballistic missiles (1)
• Boundary layer (1)
• Drag (Aerodynamics) (1)
• Rockets (Aeronautics)--Launching (1)
• Rockets (Aeronautics)--Testing (1)
• Stability of rockets (1)
• Turbulent boundary layer (1)
• Wind tunnel testing (1)

Author

• Alford, William J. (1)
• Dunning, Robert W. (1)
• King, Thomas J. (1)
• Lundstrom, Reginald R. (1)
• Silvers, H. Norman. (1)
• Ulmann, Edward F. (1)

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