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Research at NASA's NFAC wind tunnelsThe National Full-Scale Aerodynamics Complex (NFAC) is a unique combination of wind tunnels that allow the testing of aerodynamic and dynamic models at full or large scale. It can even accommodate actual aircraft with their engines running. Maintaining full-scale Reynolds numbers and testing with surface irregularities, protuberances, and control surface gaps that either closely match the full-scale or indeed are those of the full-scale aircraft help produce test data that accurately predict what can be expected from future flight investigations. This complex has grown from the venerable 40- by 80-ft wind tunnel that has served for over 40 years helping researchers obtain data to better understand the aerodynamics of a wide range of aircraft from helicopters to the space shuttle. A recent modification to the tunnel expanded its maximum speed capabilities, added a new 80- by 120-ft test section and provided extensive acoustic treatment. The modification is certain to make the NFAC an even more useful facility for NASA's ongoing research activities. A brief background is presented on the original facility and the kind of testing that has been accomplished using it through the years. A summary of the modification project and the measured capabilities of the two test sections is followed by a review of recent testing activities and of research projected for the future.
Document ID
19900016617
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Edenborough, H. Kipling
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1990
Subject Category
Aeronautics (General)
Report/Patent Number
NASA-TM-102827
NAS 1.15:102827
A-90170
Report Number: NASA-TM-102827
Report Number: NAS 1.15:102827
Report Number: A-90170
Meeting Information
Meeting: International Session of the Japan Society for Aeronautical and Space Sciences (JSASS) Aircraft Symposium
Location: Fukuoka
Country: Japan
Start Date: October 18, 1989
End Date: October 19, 1989
Accession Number
90N25933
Funding Number(s)
PROJECT: RTOP 505-61-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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