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Wind-Tunnel Procedure for Determination of Critical Stability and Control Characteristics of AirplanesThis report outlines the flight conditions that are usually critical in determining the design of components of an airplane which affect its stability and control characteristics. The wind-tunnel tests necessary to determine the pertinent data for these conditions are indicated, and the methods of computation used to translate these data into characteristics which define the flying qualities of the airplane are illustrated.
Document ID
20050241742
Acquisition Source
Headquarters
Document Type
Other - NACA Technical Report
Authors
Goett, Harry J. (National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Jackson, Roy P. (National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Belsley, Steven E. (National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1944
Subject Category
Aircraft Stability And Control
Report/Patent Number
NACA/TR-781
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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