Force and pressure tests on the GA(W)-1 airfoil with a 20-percent aileron and pressure tests with a 30-percent Fowler flap
Wentz, W. H. Seetharam, H. C. Fiscko, K. A.
Wentz, W. H.
Seetharam, H. C.
Fiscko, K. A.
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Original Date
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1976
Type
Genre
Keywords
Aerofoils,Flaps (Airplanes),Wind tunnels
Subjects (LCSH)
Citation
Wentz, W. H., et al. Force and Pressure Tests on the GA(W)-1 Airfoil with a 20-Percent Aileron and Pressure Tests with a 30-Percent Fowler Flap. Aeronautical Engineering Department, Wichita State University, 1976.
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Description
Report of research conducted under NASA grant NSG 1165, prepared by Wichita State University for NASA Langley Research Center.
Publisher
Aeronautical Engineering Department, Wichita State University
Journal
Book Title
Series
Aeronautical report (Wichita State University. Aeronautical Engineering Department)