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Effect of Mach number on the maximum lift and buffeting boundary determined in flight on a north american P-51D airplane

A limit pressure coefficient and an estimation of limit forces on airfoils at supersonic speeds

Estimation of Lift and Drag of Airfoils at Near Sonic Speeds and in the Presence of Detached Shock Waves

Published Year

• 1940-1949 (3) *

Author

• Mayer, John P. (3) *

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