Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds [microform] / John E. Lamar ... [et al.].

Format
Book
Language
English
Published/​Created
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
Description
1 v.

Available Online

Details

Related name
Series
Notes
Shipping list no.: 2003-0098-M.
Reproduction note
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2002?] 2 microfiches.
Other format(s)
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.
Other title(s)
Flight, wind tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds
SuDoc no.
NAS 1.60:210629
OCLC
51617379
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