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Influence of wall boundary layer upon the performance of an axial-flow fan rotor

Wind-tunnel investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and 0.50-airfoil chord plain sealed flaps

Published Year

• 1940-1949 (2) *

Subject

• Boundary layer (2) *
• Aerofoils (1)
• Airplanes--Control surfaces (1)
• Axial flow compressors--Blades--Aerodynamics (1)
• Flaps (Airplanes) (1)
• Wind tunnel testing (1)

Author

• Boxer, Emanuel. (1)
• Brewer, Jack D. (1)
• Polhamus, Josephine F. (1)

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