Wind tunnel tests of the GA(W)-2 airfoil with 20-percent aileron, 25-percent slotted flap, 30-percent Fowler flap and 10-percent slot-lip spoiler
Wentz, W. H.
Wentz, W. H.
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Issue Date
1976
Type
Genre
Keywords
Aerofoils,Spoilers (Airplanes),Flaps (Airplanes),Wind tunnels
Subjects (LCSH)
Citation
Wentz, W. H. Wind Tunnel Tests of the GA(W)-2 Airfoil with 20-Percent Aileron, 25-Percent Slotted Flap, 30-Percent Fowler Flap and 10-Percent Slot-Lip Spoiler. Wichita State University, 1976.
Abstract
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Description
Research conducted under NASA grant NSG 1165 for NASA Langley Research Center.
Publisher
Wichita State University
Journal
Book Title
Series
Aeronautical report (Wichita State University. Aeronautical Engineering Department)