Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
By: Wendy B. Lessard.
Contributors: Langley Research Center.
Series: NASA technical paper -- 3597.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1996
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Subsonic flow; Flow distribution; Aircraft models; Unstructured grids (Mathematics); Angle of attack; Pressure distribution; Computational fluid dynamics; Grid generation (Mathematics)
Other titles: Subsonic analysis of zero point zero four scale F-16XL models using an unstructured Euler code.
Notes: Shipping list no.: 98-0733-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.