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Guide for users of the National Transonic FacilityThe National Transonic Facility (NTF) is a fan-driven, closed-circuit, continuous flow, pressurized wind tunnel. The test section is 2.5 m x 2.5 m and 7.62 m long with a slotted-wall configuration. The NTF will have a Mach number range from 0.2 to 1.2, with Reynolds number up to 120 10 to the sixth power at Mach 1 (based on a reference length of 0.25 m). The pressure range for the facility will be from 1 to about 9 bars (1 ban = 100 kPa), and the temperature can be varied from 340 to 78 K. This report provides potential users of the NTF with the information required for preliminary planning to test programs and for preliminary layout of models and model supports which may be used in such programs.
Document ID
19810020601
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Fuller, D. E.
(NASA Langley Research Center Hampton, VA, United States)
Gloss, B. B.
(NASA Langley Research Center Hampton, VA, United States)
Nystrom, D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1981
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
L-14077
NASA-TM-83124
Report Number: L-14077
Report Number: NASA-TM-83124
Accession Number
81N29139
Funding Number(s)
PROJECT: RTOP 505-31-63-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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