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Tunnel constraint for a jet in crossflowA facet of a unified tunnel correction scheme which uses wall pressures to determine tunnel induced blockage and upwash is described. With this method, there is usually no need to use data concerning model forces or power settings to find the interference; it follows directly from the pressures and tunnel dimensions. However, highly inclined jets do not produce good pressure signatures and are highly three dimensional, so they must be treated differently. Flow modeling is also discussed.
Document ID
19850003719
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wilsden, D. J.
(Lockheed-Georgia Co. Marietta, GA, United States)
Hackett, J. E.
(Lockheed-Georgia Co. Marietta, GA, 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
85N12027
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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