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Wind-tunnel investigation of damping in roll at supersonic speeds of triangular wings at angles of attack

Wind-tunnel investigation of two vertical-takeoff-and-landing jet bomber airplane configurations at Mach numbers of 1.94 and 2.40

Published Year

• 1950-1959 (2) *

Subject

• Airplanes--Models--Testing (1)
• Airplanes--Models--Wings (1)
• Airplanes--WIngs, Triangular (1)
• Airplanes--Wings, Triangular (1)
• Charts, diagrams, etc (1)
• Rolling (Aerodynamics) (1)
• Wind tunnel testing (1)

Author

• Jones, Robert A. (2) *
• McDearmon, Russell W. (1)

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