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NASA Lewis 9- by 15-foot low-speed wind tunnel user manualThis manual describes the 9- by 15-Foot Low-Speed Wind Tunnel at the Lewis Research Center and provides information for users who wish to conduct experiments in this atmospheric facility. Tunnel variables such as pressures, temperatures, available tests section area, and Mach number ranges (0.05 to 0.20) are discussed. In addition, general support systems such as air systems, hydraulic system, hydrogen system, laser system, flow visualization system, and model support systems are described. Instrumentation and data processing and acquisition systems are also discussed.
Document ID
19940011346
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Soeder, Ronald H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1993
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-TM-106247
NAS 1.15:106247
E-7968
Report Number: NASA-TM-106247
Report Number: NAS 1.15:106247
Report Number: E-7968
Accession Number
94N15819
Funding Number(s)
PROJECT: RTOP 505-62-84
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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