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Control software for two dimensional airfoil tests using a self-streamlining flexible walled transonic test sectionOperation of the Transonic Self-Streamlining Wind Tunnel (TSWT) involved on-line data acquisition with automatic wall adjustment. A tunnel run consisted of streamlining the walls from known starting contours in iterative steps and acquiring model data. Each run performs what is described as a streamlining cycle. The associated software is presented.
Document ID
19820022438
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wolf, S. W. D. (Southampton Univ.)
Goodyer, M. J. (Southampton Univ.)
Date Acquired
September 4, 2013
Publication Date
July 1, 1982
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.26:165941
NASA-CR-165941
Report Number: NAS 1.26:165941
Report Number: NASA-CR-165941
Accession Number
82N30314
Funding Number(s)
CONTRACT_GRANT: NSG-7172
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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