Simulation of swirl in rocket nozzles at off-design pressure ratios

Keyphrases

• Nozzle 100%
• Pressure Ratio 100%
• Off-design 100%
• Rocket Nozzle 100%
• Operating Conditions 25%
• Flow Field 25%
• Shock 25%
• Computational Fluid Dynamics Simulation 25%
• Swirl Velocity 25%
• Chamber Pressure 25%
• Minor Effect 25%
• Relative Strength 25%
• Computational Domain 25%
• Revolutions per Minute 25%
• Outlet Pressure 25%
• Conical Nozzle 25%

Engineering

• Pressure Ratio 100%
• Computational Fluid Dynamics 50%
• Centerline 50%
• Chamber Pressure 50%
• Computational Domain 50%
• Relative Strength 50%
• Minor Effect 50%
• Revolutions Per Minute 50%
• Pronounced Effect 50%
• Shock Strength 50%
• Inlet Nozzle 50%
• Outlet Pressure 50%