Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds
By: John E. Lamar ... [et al.].
Contributors: Lamar, John E.; Langley Research Center.
Series: NASA/TP -- 2001-210629.; NASA technical paper -- 210629.
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from NASA Center for AeroSpace Information (CASI)
Published: 2001
Place of publication: Hampton, Va; Hanover MD
Language: eng
Format: Microform
Subjects: Aerodynamic characteristics.; Computational fluid dynamics.; Subsonic speed.; Transonic speed.; Wind tunnel tests.; Wing profiles.; Geometry.; Flight tests.; Data integration.
Other titles: Flight, wind tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds.
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.