Keyphrases
Chemical Source
33%
Chemistry Model
33%
Combustion
33%
Cross-flow Configuration
33%
Direct Integration
33%
Direct numerical Simulation
100%
Finite-rate Chemistry
100%
Hydrogen Combustion
100%
Hydrogen-air Combustion
33%
Jet in Supersonic Cross-flow
66%
Manifold Model
100%
Mixing Layer
33%
Near-wall
33%
Propulsion System
33%
Recirculation Region
66%
Reynolds-averaged Navier-Stokes
100%
Shock
33%
Shock Model
33%
Source Term
33%
Stiffness
33%
Strong Shock
33%
Strong Turbulence
33%
Tabulated Chemistry
33%
Temporal Mixing Layer
33%
Thermochemical State
33%
Turbulence Model
33%
Turbulent Combustion
33%
Water Vapor
33%
Engineering
Air Combustion
33%
Direct Numerical Simulation
100%
Jet
66%
Mixing Layer
66%
Propulsion System
33%
Reynolds-Averaged Navier-Stokes
100%
Rigidity
33%
Source Term
33%