Entry Configurations and Performance Comparisons for the Mars Smart Lander von Lockwood, Mary Kae, Powell, Richard W, Sutton, Kenneth, Prabhu, Ramadas K, Graves, Claude A, Epp, Chirold D, Carman, Gilbert L

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Experimental Hypersonic Aerodynamic Characteristics of Mars Surveyor 2001 Precision Lander with Flap von Horvath, Thomas J, O'Connell, Tod F, Cheatwood, F. McNeil, Prabhu, Ramadas K, Alter, Stephen J

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Aerodynamic Database Development for Mars Smart Lander Vehicle Configurations von Bobskill, Glenn J, Parikh, Paresh C, Prabhu, Ramadas K, Tyler, Erik D

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X-33 Aerodynamic Computations and Comparisons with Wind-Tunnel Data von Hollis, Brian R, Thompson, Richard A, Murphy, Kelly J, Nowak, Robert J, Riley, Christopher J, Wood, William A, Alter, Stephen J, Prabhu, Ramadas K

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Aerodynamic database development for Mars smart lander vehicle configurations von Bobskill, Glenn J, Parikh, Paresh C, Prabhu, Ramadas K, Tyler, Erik D

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Experimental hypersonic aerodynamic characteristics of the 2001 mars surveyor precision lander with flap von Horvath, Thomas J, Oconnell, Tod F, Cheatwood, F McNeil, Prabhu, Ramadas K, Alter, Stephen J

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Inviscid Flow Computations of Two '07 Mars Lander Aeroshell Configurations Over a Mach Number Range of 2 to 24 von Prabhu, Ramadas K.

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Inviscid Flow Computations of the Orbital Sciences X-34 Over a Mach Number Range of 1.25 to 6.0 von Prabhu, Ramadas K.

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Inviscid Flow Computations of Several Aeroshell Configurations for a '07 Mars Lander von Prabhu, Ramadas K.

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An Inviscid Computational Study of an X-33 Configuration at Hypersonic Speeds von Prabhu, Ramadas K.

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An Inviscid Computational Study of Three '07 Mars Lander Aeroshell Configurations Over a Mach Number Range of 2.3 to 4.5 von Prabhu, Ramadas K., Sutton, Kenneth

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Inviscid Flow Computations of the Shuttle Orbiter for Mach 10 and 15 and Angle of Attack 40 to 60 Degrees von Prabhu, Ramadas K., Sutton, Kenneth

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Computational Study of a McDonnell Douglas Single-Stage-to-Orbit Vehicle Concept for Aerodynamic Analysis von Prabhu, Ramadas K.

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An approximate Riemann solver for thermal and chemical nonequilibrium flows von Prabhu, Ramadas K.

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An implementation of a chemical and thermal nonequilibrium flow solver on unstructured meshes and application to blunt bodies von Prabhu, Ramadas K.

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Computational Aerodynamics of Shuttle Orbiter Damage Scenarios in Support of the Columbia Accident Investigation von Bibb, Karen L., Prabhu, Ramadas K.

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Pressure Gradient Effects on Hypersonic Cavity Flow Heating von Everhart, Joel L., Alter, Stephen J., Merski, N. Ronald, Wood, William A., Prabhu, Ramadas K.

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A rapid method for the computation of equilibrium chemical composition of air to 15 000 K / Ramadas K. Prabhu, Wayne D. Erickson von Prabhu, Ramadas K

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An Inviscid Computational Study of the Space Shuttle Orbiter and Several Damaged Configurations von Prabhu, Ramadas K., FROM, FROM, Merski, N. Ronald

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Aero-Heating of Shallow Cavities in Hypersonic Freestream Flow von Everhart, Joel L., Berger, Karen T., Merski, N. R., Jr, Woods, William A., Hollingsworth, Kevin E., Hyatt, Andrew, Prabhu, Ramadas K.

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