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An Investigation of the Aerodynamic Characteristics of an 0.08-Scale Model of the Chance Vought XF7U-1 Airplane in the Langley High-Speed 7- by 10-Foot Tunnel. Part IV - Aileron Characteristics TED No. NACA DE308: Aileron Characteristics, TED No. NACA DE308 - Part 4Tests have been conducted in the Langley high-speed 7- by 10-foot tunnel over a Mach number range from 0.40 to 0.91 to determine the stability and control characteristics of an 0.08-scale model of the Chance Vought XF7U-1 airplane. The aileron characteristics of the complete model are presented in the present report with a very limited analysis of the results.
Document ID
20050019411
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Goodson, Kenneth W. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Myers, Boyd C., II (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
August 22, 2013
Publication Date
August 22, 1947
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-RM-L7H22-Pt-4
Report Number: NACA-RM-L7H22-Pt-4
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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