Supersonic flow computations for an ASTOVL aircraft configuration
Subtitle: phase 2, part 2
By: Sekaripuram Ramakrishnan, Sukumar R. Chakravarthy, and Kuo-Yen Szema.
Contributors: Chakravarthy, Sukumar R.; Szema, Kuo-Yen.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.; Langley Research Center.
Series: NASA contractor report -- 4284.; NASA contractor report -- NASA CR-4284.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch
Published: 1990
Place of publication: [Washington, D.C.]
Language: eng
Format: Microform
Subjects: Aircraft configurations.; Computational fluid dynamics.; Design analysis.; Grid generation (Mathematics); Supersonic flow.; V/STOL aircraft.
Notes: Shipping list no.: 1991-0132-M.

"Prepared for Langley Research Center under contract NAS1-17492."

Includes bibliographical references.

Also available via Internet from the NTRS web site. Address as of 3/20/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900013430%5F1990013430.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration,] 1990. 1 microfiche.