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The US National Transonic Facility, part 1The construction of the National Transonic Facility was completed in September 1982, and checkout operations started the following month, with the maximum Reynolds number being obtained in May 1983. Following, most of the effort was devoted to installing the model access housings, and adjusting or altering various tunnel hardware systems. In May 1984, preliminary aerodynamic calibration of the tunnel was initiated in parallel with checkout of the tunnel operating systems, and in August 1984, the tunnel was declared operational and turned over to the user organization for a complete aerodynamic calibration and research and development testing. The facility has been operated in both the air and nitrogen modes covering a Mach number range of 0.2 to 1.22 at pressures up to 8.5 atm and at temperatures down to 100K. This paper presents a status of the tunnel operating systems and an overview of the major milestones during checkout.
Document ID
19860010958
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bruce, W. E., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
July 1, 1985
Publication Information
Publication: AGARD Special Course on Cryogenic Technology for Wind Tunnel Testing
Subject Category
Research And Support Facilities (Air)
Accession Number
86N20429
Distribution Limits
Public
Copyright
Other
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