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Effects of Mach number up to 0.34 and Reynolds number up to 8,000,000 on the maximum lift coefficient of a wing of NACA 66-series airfoil sections

Published Year

• 1950-1959 (1)

Subject

• Aerofoils (1)
• Airplanes--Models--Wings (1)
• Lift (Aerodynamics) (1)
• Mach number (1) *
• Reynolds number (1)

Author

• Fitzpatrick, James E. (1) *
• Furlong, G. Chester. (1)

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