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Asymptotic methods for wind tunnel wall corrections at transonic speedThe effort to develop classical methods to compute wall interference at transonic speeds is outlined. The two-dimensional theory and three-dimensional development are discussed. Also, some numerical application of the two-dimensional work are indicated. The basic advantages of the asymptotic theory are noted.
Document ID
19850003714
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Malmuth, N. D. (Rockwell International Science Center Thousand Oaks, CA, United States)
Cole, J. D. (Rockwell International Science Center Thousand Oaks, CA, United States)
Zeigler, F. (Rockwell International Science Center Thousand Oaks, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Publication Information
Publication: NASA. Langley Research Center Wind Tunnel Wall Interference Assessment and Correction, 1983
Subject Category
Aerodynamics
Accession Number
85N12022
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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