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Investigation of the effect of short fixed diffusers on starting blowdown jets in the Mach number range from 2.7 to 4.5

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

Published Year

• 1950-1959 (2) *

Subject

• Aerodynamics, Supersonic (1)
• Airplanes--Wings, Swept-back (1)
• Airplanes--Wings, Triangular (1)
• Airplanes--Wings--Testing (1)
• Charts, diagrams, etc (1)
• Pitching (Aerodynamics) (1)

Author

• Moore, John A. (2) *

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