Numerical analysis of water phase transition effects in combustion-heated wind tunnels

Engineering

• Nozzle Exit 100%
• Low-Temperature 50%
• Inviscid Flow 50%
• Liquid Droplet 50%
• Flow Condition 50%
• Number Density 50%
• Source Term 50%
• Mass Fraction 50%
• Model Experiment 50%
• Droplet Growth 50%
• Static Temperature 50%
• Test Section 50%
• Condensation Shock 50%
• Homogeneous Nucleation 50%
• Oblique Shock 50%
• Exit Mach Number 50%
• Flow Property 50%
• Flow Parameters 50%
• Mach Number 50%
• Nonequilibrium 50%
• Numerical Methods 50%
• Latent Heat 50%
• Static Pressure 50%

Keyphrases

• Water Phase Transition 100%
• Combustion-heated Wind Tunnel 100%
• Water Analysis 100%
• Exit Mach number 16%
• Non-equilibrium Condensation 16%
• Gas Effect 16%
• Condensation Shock 16%
• Tunnel Test 16%
• Equilibrium Evaporation 16%
• Oblique Shock 16%
• Hypersonic Flight 16%
• Outflow Problem 16%
• Long Nozzle 16%