An edition of Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds (2001)

Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds

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Flight, wind-tunnel, and computational fluid ...
John E. Lamar
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Last edited by MARC Bot
December 14, 2024 | History
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An edition of Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds (2001)

Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds

by

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Publish Date
Publisher
National Aeronautics and Space Administration, Langley Research Center, Available from NASA Center for AeroSpace Information (CASI)
Language
English

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Subjects

Aerodynamics, Aerodynamic characteristics, Computational fluid dynamics, Subsonic speed, Transonic speed, Wind tunnel tests, Wing profiles, Geometry, Flight tests, Data integration
Edition Availability
Cover of: Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds
Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds
2001, National Aeronautics and Space Administration, Langley Research Center, Available from NASA Center for AeroSpace Information (CASI)
in English

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Book Details

Edition Notes

Shipping list no.: 2003-0098-M.

Also available via Internet from the NASA web site. Address as of 2/10/03: http://techreports.larc.nasa.gov/ltrs/PDF/2001/tp/NASA-2001-tp210629.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2002?] 2 microfiches.

System requirements: Adobe Acrobat Reader.

Published in
Hampton, Va, Hanover MD
Series
NASA/TP -- 2001-210629., NASA technical paper -- 210629.
Other Titles
Flight, wind tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds.

The Physical Object

Pagination
1 v.

Edition Identifiers

Open Library
OL17610253M
OCLC/WorldCat
51617379

Work Identifiers

Work ID
OL18528281W

Source records

Oregon Libraries MARC record
harvard_bibliographic_metadata record

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History

Download catalog record: RDF / JSON
December 14, 2024 Edited by MARC Bot import existing book
February 8, 2019 Created by MARC Bot import existing book