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Transonic assessment of two-dimensional wind tunnel wall interference using measured wall pressuresA method is described for assessing wall interference in two dimensional wind tunnels with better realism and accuracy than is achieved with methods based on classical wall interference theory. Measured pressure distributions were imposed as boundary conditions on a nonlinear transonic form of the potential equation to obtain an accurate computational reproduction of the actual tunnel flow. Wall-induced velocity perturbations were then extracted to yield both corrections to the tunnel test conditions and a measure of the adequacy of these corrections to account for tunnel interference. Application of the method to a transonic tunnel with variable porosity walls is illustrated.
Document ID
19790011820
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kemp, W. B., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Publication Information
Publication: Advanced Technol. Airfoil Res., Vol. 1, Pt. 2
Subject Category
Research And Support Facilities (Air)
Accession Number
79N19991
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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