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Direct calculation of wall interferences and wall adaptation for two-dimensional flow in wind tunnels with closed wallsA method for the direct calculation of the wall induced interference velocity in two dimensional flow based on Cauchy's integral formula was derived. This one-step method allows the calculation of the residual corrections and the required wall adaptation for interference-free flow starting from the wall pressure distribution without any model representation. Demonstrated applications are given.
Document ID
19870005803
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Amecke, Juergen
(NASA Headquarters Washington, DC United States)
Date Acquired
September 5, 2013
Publication Date
December 1, 1986
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.15:88523
NASA-TM-88523
Report Number: NAS 1.15:88523
Report Number: NASA-TM-88523
Accession Number
87N15236
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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