QCT-based vibrational collisional models applied to nonequilibrium nozzle flows

Keyphrases

• Non-equilibrium 100%
• Rate Coefficients 100%
• Vibrational Levels 100%
• Nozzle Flow 100%
• NASA Ames 100%
• Collisional Models 100%
• Governing Equation 50%
• Dissociation 50%
• Discretized 50%
• Rotation Mode 50%
• Low-lying States 50%
• Non-equilibrium Effects 50%
• Quasi-1D 50%
• Steady-state Solution 50%
• Level Dynamics 50%
• Translational Mode 50%
• Finite Volume Method 50%
• Inviscid 50%
• Boltzmann Distribution 50%
• Implicit Time Integration Methods 50%
• Ro-vibrational 50%
• Thermal Non-equilibrium 50%
• Expanding Flow 50%
• Chemical Non-equilibrium 50%
• Fully Implicit Time Integration 50%
• Chemical Databases 50%
• Hypersonic Nozzle 50%
• High-lying States 50%

Engineering

• Nonequilibrium 100%
• NASA 100%
• Flow in Nozzles 100%
• Good Agreement 50%
• Acquired Data 50%
• Experimental Result 50%
• Rotational 50%
• State Solution 50%
• Integration Method 50%
• Implicit Time 50%
• Finite Volume Method 50%
• Boltzmann Distribution 50%

Physics

• Steady State 100%
• Boltzmann Distribution 100%
• Hypersonics 100%
• Nozzle Flow 100%