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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
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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)