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Tunnel Correction for Compressible Subsonic FlowThis report presents a treatment of the effects of the tunnel walls on the flow velocity and direction in a compressible medium at subsonic speed by an approximate method. Calculations are given for the rotationally symmetric and two- dimensionl problems of the flow past bodies, as well for the downwash effect in the tunnel with circular cross section.
Document ID
20040015218
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Baranoff, A. V. (National Advisory Committee for Aeronautics Washington, DC, United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 1947
Subject Category
Numerical Analysis
Report/Patent Number
NACA-TM-1162
Report Number: NACA-TM-1162
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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