Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoiler
Wentz, W. H. Fiscko, K. A.
Wentz, W. H.
Fiscko, K. A.
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1977
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Keywords
Aerofoils,Wind tunnels
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Citation
Wentz, W. H., and K. A. Fiscko. Wind Tunnel Force and Pressure Tests of a 21% Thick General Aviation Airfoil with 20% Aileron, 25% Slotted Flap and 10% Slot-Lip Spoiler. Wichita State University, [Aeronautical Engineering Department], 1977.
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Report of research conducted under NASA grant NSG 1165.;Prepared by Wichita State University for NASA Langley Research Center.
Publisher
Wichita State University, [Aeronautical Engineering Department], :
Journal
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Series
Aeronautical report (Wichita State University. Aeronautical Engineering Department)