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Last edited by ImportBot
September 19, 2008 | History

Ramadas K. Prabhu

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  • Cover of: An inviscid computational study of an X-33 configuration at hypersonic speeds

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  • Cover of: inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5

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  • Cover of: Inviscid flow computations of several aeroshell configurations for a '07 Mars lander

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  • Cover of: Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0

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  • Cover of: A rapid method for the computation of equilibrium chemical composition of air to 15 000 K

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  • Cover of: Summary report of the orbital X-34 wing static aeroelastic study

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  • Cover of: An approximate Riemann solver for thermal and chemical nonequilibrium flows

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  • Cover of: An implementation of a chemical and thermal nonequilibrium flow solver on unstructured meshes and application to blunt bodies

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  • Cover of: Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis

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  • Cover of: Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees

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

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  • Cover of: Studies on the interference of wings and propeller slipstreams: final report for the period ending December 31, 1984

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History

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September 19, 2008 Created by ImportBot Imported from Oregon Libraries MARC record