Computational Analysis of the Oxidizer Preflow in an Upper-Stage Rocket Engine

Volume 25, Number 3May 2009

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Topics

• Aircraft Engines
• Combustion Chambers
• Convection
• Energy
• Energy Conversion
• Energy Forms, Production and Conversion
• Enthalpy
• Heat Conduction
• Heat Engines
• Heat Transfer
• Heating, Ventilating, and Air Conditioning
• Internal Combustion Engines
• Mass Transfer
• Propulsion and Power
• Thermodynamic Properties
• Thermodynamics
• Thermophysical Properties
• Thermophysics and Heat Transfer

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Keywords

• Aestus
• Chamber Pressure
• Reynolds Averaged Navier Stokes
• Conjugate Heat Transfer Analysis
• Flow Conditions
• Bipropellants
• Aerodynamic Force
• Wall Temperature
• Mass Flow Rate
• Divergent Nozzles

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Digital

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• Published online23 May 2012