Transonic aerodynamics including strong effects from heat addition

Keyphrases

• Heat Addition 100%
• Transonic Flow 100%
• Transonic Aerodynamics 100%
• Mach number 66%
• Flow Field 66%
• Phase Transition 66%
• Condensation Process 66%
• Gas Mixture 66%
• Heat Release 66%
• Homogeneous nucleation 66%
• Airfoil 66%
• Inviscid Flow 66%
• Carrier Gas 66%
• Nonequilibrium Phase Transitions 66%
• Pressure Drag 66%
• Atmospheric Flight 66%
• Shock Tube 33%
• Shear Layer 33%
• Shock 33%
• Water Vapor 33%
• Growth Law 33%
• Cooling Rate 33%
• Condensation 33%
• Mixed Vapor 33%
• Vapor Pressure 33%
• Finite Volume Method 33%
• Heat Shock 33%
• Wind Tunnel 33%
• Angle of Attack 33%
• Wing Section 33%
• Numerical Code 33%
• Free Stream 33%
• Reservoir Conditions 33%
• Near-equilibrium 33%
• Turbulent Boundary Layers 33%
• Water Flow 33%
• Viscous Effects 33%
• Gas Dynamics 33%
• Coupled Processes 33%
• Euler Equations 33%
• Heat Source Distribution 33%
• Classical nucleation Theory 33%
• Droplet Growth 33%
• Nucleation Zone 33%
• Pure Vapour 33%
• Flight Flow 33%
• Nitrogen Vapor 33%
• Cryogenic Wind Tunnel 33%
• Airplane Wing 33%
• Fluid Components 33%

Engineering

• Stronger Effect 100%
• Transonic Flow 100%
• Heat Addition 100%
• Aerodynamics 100%
• Heat Release 66%
• Homogeneous Nucleation 66%
• Carrier Gas 66%
• Condensation Process 66%
• Nonequilibrium 66%
• Airfoil 66%
• Pressure Drag 66%
• Flow Distribution 66%
• Inviscid Flow 66%
• Gas Mixture 66%
• Tunnel 66%
• Mach Number 33%
• Shear Layer 33%
• Aircraft 33%
• Cooling Rate 33%
• Angle-of-Attack 33%
• Finite Volume Method 33%
• Reservoir Condition 33%
• Turbulent Boundary Layer 33%
• Free-Stream Mach Number 33%
• Classical Nucleation Theory 33%
• Droplet Growth 33%
• Euler Equation 33%
• Pure Vapor 33%
• Boundary Layer Calculation 33%
• Actuator 33%
• Heat Sources 33%
• Coupling 33%