Numerical simulation of rocket nozzle

Engineering

• Performance Parameter 100%
• Divergence Angle 100%
• Mach Number 100%
• Pressure Ratio 100%
• Computer Simulation 100%
• Computational Fluid Dynamics 50%
• Flow Rate 50%
• Rate Distribution 50%
• Exit Pressure 50%
• Flow Pressure 50%
• Area Ratio 50%
• Diverging Nozzle 50%
• Ansys Fluent 50%
• Discharge Coefficient 50%
• Static Pressure 50%
• Inlet Pressure 50%
• Pressure Distribution 50%
• Flow Velocity 50%
• Coordinates 50%

INIS

• nozzles 100%
• computerized simulation 100%
• rockets 100%
• performance 33%
• mach number 33%
• computer codes 16%
• increasing 16%
• distribution 16%
• geometry 16%
• flow rate 16%
• simulation 16%
• surveys 16%
• throat 16%
• vents 16%
• computational fluid dynamics 16%
• turbulence 16%