Validation of Computational Fluid Dynamics for supersonic Shock containing jets

Keyphrases

• Axisymmetric Nozzle 33%
• Broadband Shock-associated Noise 66%
• Computational Fluid Dynamics 100%
• Computational Fluid Dynamics Simulation 33%
• Contour Plots 33%
• Flow Field 33%
• Further Analysis 33%
• Mach number 33%
• Model-driven Development 33%
• Navier-Stokes Solver 33%
• Noise Model 33%
• Noise Source 33%
• Off-design 66%
• Over-under 33%
• Pitot Pressure 33%
• Pitot-Static 33%
• Pressure Probe 33%
• Reynolds-averaged Navier-Stokes 33%
• Shock 100%
• Source Strength 33%
• Static Pressure 66%
• Steady State 33%
• Supersonic Jet 33%
• Two-equation Turbulence Model 33%
• Under-expanded 66%

Engineering

• Axisymmetric 50%
• Computational Fluid Dynamics 100%
• Contour Plot 25%
• Design Parameter 25%
• Downstream Location 25%
• Equation Turbulence Model 25%
• Experimental Result 25%
• Mach Number 25%
• Noise Source 25%
• Pressure Probe 25%
• Pressure Sensor 25%
• Reynolds-Averaged Navier-Stokes 25%
• Schlieren 25%
• Source Strength 25%
• Static Pressure 50%