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The Basic Aerodynamics Research Tunnel - A facility dedicated to code validationComputational fluid dynamics code validation requirements are discussed together with the need for close interaction between experiment and code development. Code validation experiments require a great deal of data and for the experiments to be successful, a highly-productive research facility is required. A description is provided of the NASA Langley Basic Aerodynamics Research Tunnel (BART); especially the instrumentation and experimental techniques that make the facility ideally suited to code validation experiments. Results are presented from recent tests which illustrate the techniques used in BART.
Document ID
19880050683
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sellers, William L., III
(NASA Langley Research Center Hampton, VA, United States)
Kjelgaard, Scott O.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 88-1997
Report Number: AIAA PAPER 88-1997
Meeting Information
Meeting: Aerodynamic Testing Conference
Location: San Diego, CA
Country: United States
Start Date: May 18, 1988
End Date: May 20, 1988
Sponsors: AIAA
Accession Number
88A37910
Distribution Limits
Public
Copyright
Other

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