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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
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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)
