Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
By: Ramadas K. Prabhu ; [prepared ... under contract NAS1-96014].
Contributors: Langley Research Center.
Series: [NASA contractor report] -- NASA/CR-2001-210849.; NASA contractor report -- NASA CR-210849.
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: Inviscid flow.; Viscous flow.; Computational fluid dynamics.; Aerodynamic loads.; Hypersonic speed.; Supersonic speed.
Notes: Shipping list no.: 2002-0173-M.

"April 2001."

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