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ramadas k prabhu

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Supersonic speedInviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0Ramadas K. Prabhu

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

Ramadas K. Prabhu · Available from NASA Center for Aerospace Information

Sayfa sayısı yok · 2001

Inviscid flow / Viscous flow / Hypersonic speed / Aerodynamic loads / Supersonic speed

Aerodynamic characteristicsInviscid flow computations of several aeroshell configurations for a '07 Mars landerRamadas K. Prabhu

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

Ramadas K. Prabhu · Available from NASA Center for Aerospace Information

Sayfa sayısı yok · 2001

Aeroshells / Inviscid flow / Aerodynamic characteristics

Wind tunnel testsAn inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5Ramadas K. Prabhu

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

Ramadas K. Prabhu · National Aeronautics and Space Administration, Langley Research Center

Sayfa sayısı yok · 2001

Aeroshells / Computational fluid dynamics / Mars missions / Aerodynamics / Wind tunnel tests

Aerodynamic characteristicsSummary report of the orbital X-34 wing static aeroelastic studyRamadas K. Prabhu

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

Ramadas K. Prabhu · National Aeronautics and Science Administration, Langley Research Center

Sayfa sayısı yok · 2001

Inviscid flow / Computational fluid dynamics / Free flow / X-34 reusable launch vehicle / Aerodynamic characteristics

AnalysisA rapid method for the computation of equilibrium chemical composition of air to 15 000 KRamadas K. Prabhu

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

Ramadas K. Prabhu · National Aeronautics and Space Administration, Scientific and Technical Information Division

28 sayfa · 1988

High temperature air / Equilibrium air / Chemical composition / Thermodynamic properties / Analysis

Venturestar launch vehicleAn inviscid computational study of an X-33 configuration at hypersonic speedsRamadas K. Prabhu

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

Ramadas K. Prabhu · National Aeronautics and Space Administration, Langley Research Center

Sayfa sayısı yok · 1999

Computational fluid dynamics / Inviscid flow / Viscous flow / X-33 reusable launch vehicle / Venturestar launch vehicle

Blunt bodiesAn implementation of a chemical and thermal nonequilibrium flow solver on unstructured meshes and application to blunt bodiesRamadas K. Prabhu

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

Ramadas K. Prabhu · National Aeronautics and Space Administration, Langley Research Center

Sayfa sayısı yok · 1994

Nonequilibrium flow / Vibration / Hypersonic flow / Cylindrical bodies / Blunt bodies

Angle of attackInviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degreesRamadas K. Prabhu

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

Ramadas K. Prabhu · National Aeronautics and Science Administration, Langley Research Center

Sayfa sayısı yok · 2001

Computational fluid dynamics / Inviscid flow / Aerodynamic coefficients / Space shuttle orbiters / Angle of attack

Spacecraft structuresInviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24Ramadas K. Prabhu

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

Ramadas K. Prabhu · Available from NASA Center for Aerospace Information

Sayfa sayısı yok · 2001

Computational fluid dynamics / Inviscid flow / Aeroshells / Spacecraft structures

Hypersonic flowComputational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysisRamadas K. Prabhu

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

Ramadas K. Prabhu · National Aeronautics and Space Administration, Langley Research Center

Sayfa sayısı yok · 1996

Aerodynamic characteristics / Applications programs (Computers) / Computational grids / Finite element method / Hypersonic flow

WingsStudies on the interference of wings and propeller slipstreamsRamadas K. Prabhu

Studies on the interference of wings and propeller slipstreams

Ramadas K. Prabhu · Old Dominion University Research Foundation

Sayfa sayısı yok · 1985

Airplanes / Wings

Gas flowAn approximate Riemann solver for thermal and chemical nonequilibrium flowsRamadas K. Prabhu

An approximate Riemann solver for thermal and chemical nonequilibrium flows

Ramadas K. Prabhu · National Technical Information Service, distributor

Sayfa sayısı yok · 1994

Computational fluid dynamics / Inviscid flow / Aerothermodynamics / Nonequilibrium flow / Gas flow