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A low speed two-dimensional study of flow separation on the GA(W)- 1 airfoil with 30-percent chord Fowler flap

Seetharam, H. C.
; 
Wentz, W. H.
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Authors
Seetharam, H. C.
Wentz, W. H.
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1976
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Keywords
Aerofoils,Flaps (Airplanes),Skin friction (Aerodynamics),Turbulent boundary layer
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Citation
Seetharam, H. C., and W. H. Wentz. A Low Speed Two-Dimensional Study of Flow Separation on the GA(W)- 1 Airfoil with 30-Percent Chord Fowler Flap. Aeronautical Engineering Department, Wichita State University, 1976.
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Description
Final technical report of research conducted under NGR-17-003-02 Phase II, for the NASA Langley Research Center.
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Aeronautical Engineering Department, Wichita State University
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Aeronautical report (Wichita State University. Aeronautical Engineering Department)
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https://hdl.handle.net/10057/27248
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WSU Books (1964-current year)
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