Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24

An edition of Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24 (2001)

Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24

By Ramadas K. Prabhu

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Publish Date

2001

Publisher

National Aeronautics and Science Administration, Langley Research Center,Available from NASA Center for Aerospace Information

Language

eng

Pages

Description:

subjects: Computational fluid dynamics, Inviscid flow, Aeroshells, Spacecraft structures