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Transonic wind-tunnel wall interferenceA method for analyzing wall interference is described which avoids the assumption of linear superposition of perturbations in extracting the wall induced velocity field. Measurements of pressure distribution on or near the tunnel walls during the actual wind tunnel test, are imposed as boundary values to be matched. Instead of applying wall interference corrections to the wind tunnel data, some property of the wall is adjusted until a calculated interference free criterion is satisfied for each tunnel data point. The mode of operation for the National Transonic Facility, envisioned as a correctable interference transonic tunnel, combines the capability for accurate assessment of wall interference with a limited capability for wall control.
Document ID
19770020199
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kemp, W. B., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1977
Publication Information
Publication: High Reynolds Number Res.
Subject Category
Research And Support Facilities (Air)
Accession Number
77N27143
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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