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Research on self-correcting wind tunnelsThe Calspan self-correcting wind tunnel is a two-dimensional facility in which the flow field in the vicinity of the walls is actively controlled, and a theoretical evaluation is used in conjunction with flow field measurements to confirm that wall interference was minimized. The facility is described, and the results of experiments with a 6 percent-blockage model are presented to show that iterative application of wall control effectively eliminates the interference. Experiments were performed at conditions where the flow at the walls was supercritical, and a new operating procedure is described for these conditions. The results of an analysis of the flow in the auxiliary suction system and test ion illustrate the tradeoffs available in the design of self-correcting wind tunnel test sections and in model sizing for such tunnels.
Document ID
19790011821
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vidal, R. J.
(Calspan Corp. Buffalo, NY, United States)
Erickson, J. C., Jr.
(Calspan Corp. Buffalo, NY, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Publication Information
Publication: NASA. Langley Res. Center Advanced Technol. Airfoil Res., Vol. 1, Pt. 2
Subject Category
Research And Support Facilities (Air)
Accession Number
79N19992
Funding Number(s)
CONTRACT_GRANT: F40600-76-C-0011
CONTRACT_GRANT: N00014-72-C-0102
CONTRACT_GRANT: N00014-77-C-0052
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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