Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24
By: Ramadas K. Prabhu ; [prepared ... under contract NAS1-00135].
Contributors: Langley Research Center.
Series: [NASA contractor report] -- NASA/CR-2001-210852.; NASA contractor report -- NASA CR-210852.
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: Computational fluid dynamics.; Inviscid flow.; Aeroshells.; Spacecraft structures.
Notes: Shipping list no.: 2002-0173-M.

"April 2001."

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