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Wall effects in wind tunnelsA synthesis of current trends in the reduction and computation of wall effects is presented. Some of the points discussed include: (1) for the two-dimensional, transonic tests, various control techniques of boundary conditions are used with adaptive walls offering high precision in determining reference conditions and residual corrections. A reduction in the boundary layer effects of the lateral walls is obtained at T2; (2) for the three-dimensional tests, the methods for the reduction of wall effects are still seldom applied due to a lesser need and to their complexity; (3) the supports holding the model of the probes have to be taken into account in the estimation of perturbatory effects.
Document ID
19860018625
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chevallier, J. P.
(NASA Headquarters Washington, DC United States)
Vaucheret, X.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1986
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.15:88447
NASA-TM-88447
Report Number: NAS 1.15:88447
Report Number: NASA-TM-88447
Accession Number
86N28097
Funding Number(s)
CONTRACT_GRANT: NASW-4005
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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