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Development in UK of a method for calculating tunnel wall corrections from flow measurementsClassical methods for calculation of wall corrections which are not satisfactory for a number of flows of interest are discussed. To meet these objections, a number of methods were developed which use measurements of the low at or close to the tunnel walls as an outer boundary condition to define wall interference. The development, assessment and application of one such method is summarized.
Document ID
19850003718
Acquisition Source
Legacy CDMS
Document Type
Contribution to a larger work
Authors
P. R. Ashill (Royal Aircraft Establishment Bedford, United Kingdom)
Date Acquired
August 12, 2013
Publication Date
January 1, 1983
Publication Information
Publication: Wind Tunnel Wall Interference Assessment and Correction, 1983
Publisher: National Aeronautics and Space Administration
Subject Category
Aerodynamics
Accession Number
85N12026
Funding Number(s)
PROJECT: RTOP 505-31-53-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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