Computational analysis of the oxidizer preflow in an upper-stage rocket engine

INIS

• sprays 100%
• rocket engines 100%
• oxidizers 100%
• distribution 60%
• deposits 40%
• droplets 40%
• liquids 40%
• walls 40%
• combustion chambers 40%
• transfer functions 20%
• injection 20%
• dynamics 20%
• levels 20%
• parametric analysis 20%
• accounting 20%
• source terms 20%
• numerical solution 20%
• coupling 20%
• atomization 20%
• interactions 20%
• vapors 20%
• propellants 20%
• low pressure 20%
• nozzles 20%
• evaporation 20%
• size 20%
• experimental data 20%
• iterative methods 20%

Engineering

• Computational Analysis 100%
• Stage Rocket 100%
• Combustion Chamber 66%
• Solution Procedure 33%
• Pressure Flow 33%
• Droplet Size Distribution 33%
• Couplings 33%
• Lagrange 33%
• Atomisation 33%
• Linearization 33%
• Nozzle 33%
• Flow Regime 33%
• Two Dimensional 33%
• Chamber Wall 33%
• Parametric Study 33%
• Superheated Liquid 33%
• Source Term 33%

Material Science

• Temperature 100%
• Liquid 100%
• Droplet 100%
• Nozzle 50%
• Vapor 50%
• Atomizer Nozzle 50%