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TWINTAN: A program for transonic wall interference assessment in two-dimensional wind tunnelsA method for assessing the wall interference in transonic two dimensional wind tunnel test was developed and implemented in a computer program. The method involves three successive solutions of the transonic small disturbance potential equation to define the wind tunnel flow, the perturbation attriburable to the model, and the equivalent free air flow around the model. Input includes pressure distributions on the model and along the top and bottom tunnel walls which are used as boundary conditions for the wind tunnel flow. The wall induced perturbation fields is determined as the difference between the perturbation in the tunnel flow solution and the perturbation attributable to the model. The methodology used in the program is described and detailed descriptions of the computer program input and output are presented. Input and output for a sample case are given.
Document ID
19800014843
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kemp, W. B., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1980
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-TM-81819
Accession Number
80N23332
Funding Number(s)
PROJECT: RTOP 505-31-53-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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