Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees
By: Ramadas K. Prabhu.
Contributors: Langley Research Center.
Series: [NASA contractor report] -- NASA/CR-2001-211267.; NASA contractor report -- NASA CR-211267.
Publisher: National Aeronautics and Science Administration, Langley Research Center; Available from NASA Center for Aerospace Information
Published: 2001
Place of publication: Hampton, Va; Hanover, MD
Language: eng
Format: Microform
Subjects: Aerodynamic characteristics.; Aerodynamic coefficients.; Angle of attack.; Computational fluid dynamics.; Hypersonic speed.; Inviscid flow.; Mach number.; Space shuttle orbiters.
Notes: Shipping list no.: 2002-0546-M.

"December 2001."

Also available via Internet from the NASA Web site. Address as of 2/21/04: http://techreports.larc.nasa.gov/ltrs/PDF/2001/cr/NASA-2001-cr211267.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2002?]. 1 microfiche.