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User's manual for a 0.3-m TCT wall interference assessment/correction procedure: 8- by 24-inch airfoil test sectionA transonic Wall-Interference Assessment/Correction (WIAC) procedure has been developed and verified for the 8- by 24-inch airfoil test section of the Langley 0.3-m Transonic Cryogenic Tunnel. This report is a user's manual for the correction procedure. It includes a listing of the computer procedure file as well as input for and results from a step-by-step sample case.
Document ID
19860001722
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Gumbert, C. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:87582
NASA-TM-87582
Report Number: NAS 1.15:87582
Report Number: NASA-TM-87582
Accession Number
86N11189
Funding Number(s)
PROJECT: RTOP 505-31-53-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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