Two-temperature plasma modeling of nitrogen/hydrogen arcjets

Engineering

• Axisymmetric Flow 50%
• Boundary Layer 50%
• Centerline 50%
• Continuity Equation 50%
• Current Distribution 100%
• Electrical Conductivity 50%
• Electron Temperature 50%
• Energy Equation 50%
• Equilibrium Model 50%
• Heavy Specie 50%
• Momentum Equation 50%
• Nonequilibrium 50%
• Numerical Solution 50%
• Plasma Modeling 100%
• Plasma Property 50%
• Strong Electric Field 50%
• Temperature Distribution 50%
• Temperature Plasma 100%
• Thermal Equilibrium 50%
• Thruster 100%

Keyphrases

• Anode Temperature 25%
• Arcjet 100%
• Arcjet Thruster 25%
• Axisymmetric Flow 25%
• Boundary Layer 25%
• Chemical Equilibrium Model 25%
• Constrictor 25%
• Continuity Equation 25%
• Current Distribution 50%
• Electrical Conduction 25%
• Electrical Conductivity 25%
• Electron Temperature 25%
• Energy Equation 25%
• Flow Field 25%
• Hydrazine 25%
• Hydrogen Plasma 25%
• Ion Levels 25%
• Low Power 25%
• Momentum Equation 25%
• Nozzle 25%
• Numerical Results 25%
• Numerical Solution 25%
• Plasma Composition 25%
• Plasma Current 25%
• Plasma Modeling 100%
• Plasma Properties 25%
• Propellant 50%
• Strong Electric Field 25%
• Temperature Approach 25%
• Temperature Distribution 25%
• Thermal Equilibrium 25%
• Thermal Non-equilibrium 25%
• Thruster 25%
• Two-temperature 50%
• Two-temperature Plasma 100%