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Empty test section streamlining of the transonic self-streamlining wind tunnel fitted with new wallsThe original flexible top and bottom walls of the Transonic Self-Streamlining Wind Tunnel (TSWT), at the University of Southampton, have been replaced with new walls featuring a larger number of static pressure tappings and detailed mechanical improvements. This report describes the streamling method, results, and conclusions of a series of tests aimed at defining sets of aerodynamically straight wall contours for the new flexible walls. This procedure is a necessary prelude to model testing. The quality of data obtained compares favorably with the aerodynamically straight data obtained with the old walls. No operational difficulties were experienced with the new walls.
Document ID
19880016058
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lewis, M. C.
(Southampton Univ.)
Date Acquired
September 5, 2013
Publication Date
July 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
AASU-MEMO-86/10
NAS 1.26:181680
NASA-CR-181680
Report Number: AASU-MEMO-86/10
Report Number: NAS 1.26:181680
Report Number: NASA-CR-181680
Accession Number
88N25442
Funding Number(s)
CONTRACT_GRANT: NSG-7172
PROJECT: RTOP 505-61-01-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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