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Streamlining the walls of an empty two-dimensional flexible-walled test sectionThe techniques used to find aerodynamically straight wall contours in a test section of a transonic wind tunnel are discussed. The walls were defined as aerodynamically straight up to Mach 0.9.
Document ID
19820020428
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wolf, S. W. D. (Southampton Univ.)
Goodyer, M. J. (Southampton Univ.)
Cook, I. D. (Southampton Univ.)
Date Acquired
September 4, 2013
Publication Date
May 1, 1982
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.26:165936
NASA-CR-165936
Report Number: NAS 1.26:165936
Report Number: NASA-CR-165936
Accession Number
82N28304
Funding Number(s)
CONTRACT_GRANT: NSG-7172
PROJECT: RTOP 505-31-43-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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