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Effects of Compressibility on the Flow Past Thick Airfoil Sections

Effects of Compressibility on the Characteristics of Five Airfoils

Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 to 20 degrees at high subsonic speeds

Published Year

• 1940-1949 (3) *

Subject

• Aerofoils--Testing (1)
• Angle of attack (Aerodynamics) (1)
• Charts, diagrams, etc (1)
• Schlieren photography (1)
• Wind tunnel testing (1)

Author

• Daley, Bernard N. (3) *
• Lord, Douglas R. (1)

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