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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 I - Basic Longitudinal Stability Characteristics, TED No. NACA DE308: Basic Longitudinal Stability Characteristics, TED No. NACA DE308 - Part 1The stability and control characteristics of an 0.08-scale model of the Chance Vought XF7U-1 airplane have been investigated over a Mach number range from 0.40 to 0.91. Results of the basic longitudinal tests of the complete model with undeflected control surfaces are given in the present report with a very limited analysis of the results.
Document ID
20050019437
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Kemp, William B., Jr. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Kuhn, Richard E. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Goodson, Kenneth W. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
August 22, 2013
Publication Date
July 18, 1947
Subject Category
Aircraft Stability And Control
Report/Patent Number
NACA-RM-L7G08-Pt-1
Report Number: NACA-RM-L7G08-Pt-1
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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