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
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Authors
Wentz, W. H.
Advisors
Issue Date
1976
Type
Keywords
Aerofoils , Spoilers (Airplanes) , Flaps (Airplanes) , Wind tunnels
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
Table of Contents
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)