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An inerference assessment approach for a three-dimensional slotted tunnel with sparse wall pressure dataThe various procedures referred to as wall interference assessment and correction procedures presume the existence of a surface distribution of data (usually static pressure) measured over a surface on or near the tunnel walls for each test point to be assessed. An alternative approach in which a reasonably sophisticated computer model of the test section flow would be fitted parametrically to a sparse set of measured data is presented. The measurements provides line distributions of static pressure near the center lines of the top, side and bottom walls. The development of a test section model incorporating explicit recognition of discrete slots of finite length with controlled flow reentry into the solid wall downstream portion of the tunnel is shown.
Document ID
19850003722
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kemp, W. B., Jr.
(Virginia Associated Research Center Newport News, VA, 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
85N12030
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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