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The F2 wind tunnel at Fauga-MauzacDetails on the French subsonic wind-tunnel F2 that becomes operational on July 1983 are presented. Some of the requirements were: (1) installation of models on any wall of the facility, (2) good observation points due to transparent walls, (3) smooth flow, (4) a laser velocimeter, and (5) easy access and handling. The characteristics include a nonpressurized return circuit, dimensions of 5 x 1.4 x 1.8 m, maximum velocity of 100 m/s and a variable speed fan of 683 kW.
Document ID
19840020745
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Afchain, D. (NASA Headquarters Washington, DC United States)
Broussaud, P. (NASA Headquarters Washington, DC United States)
Frugier, M. (NASA Headquarters Washington, DC United States)
Rancarani, G. (NASA Headquarters Washington, DC United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1984
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.15:77482
NASA-TM-77482
Meeting Information
Meeting: Colloq. d''Aerodyn. Appl.
Location: Toulouse
Country: France
Start Date: November 8, 1983
End Date: November 10, 1983
Accession Number
84N28814
Funding Number(s)
CONTRACT_GRANT: NASW-3541
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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