Optimization of the aerodynamic flame stabilization for fuel flexible gas turbine premix burners

Keyphrases

• Flame Stabilization 100%
• Aerodynamics 100%
• Combustion 100%
• Gas Turbine 100%
• Burner 100%
• Premixed 100%
• Vortex Breakdown 100%
• Swirling Flow 100%
• Flex-fuel Vehicles 100%
• Flame Flashback 66%
• Induced Vortex 66%
• Azimuthal Vorticity 66%
• Combustion Chamber 33%
• Combustor 33%
• Flow Field 33%
• Cross-sectional Area 33%
• Strong Interaction 33%
• Fluid Mechanics 33%
• Area Change 33%
• Fixed Position 33%
• Flow Effect 33%
• Flame Stability 33%
• Gas Turbine Combustor 33%
• Vortex Dynamics 33%
• Aerodynamic Design 33%
• Recirculation Zone 33%
• Core Flow 33%
• Premixed Combustion 33%
• Local Extinction 33%
• Flame Propagation 33%
• Swirler 33%
• Vorticity Transport Equation 33%
• Low-emission Combustor 33%
• Central Recirculation Zone 33%
• Sudden Transition 33%
• Optimized Tailoring 33%
• Fire Chemistry 33%

Engineering

• Gas Turbine 100%
• Vortex 100%
• Swirling Flow 100%
• Vorticity 100%
• Aerodynamics 100%
• Azimuthal 66%
• Recirculation Zone 66%
• Combustion Chamber 66%
• Combustor 33%
• Gas Turbine Combustors 33%
• Strong Interaction 33%
• Aerodynamic Design 33%
• Fluid Mechanics 33%
• Core Flow 33%
• Premixed Combustion 33%
• Fixed Position 33%
• Flame Propagation 33%
• Flame Stability 33%
• Flow Distribution 33%
• Vortex Dynamics 33%
• Centerline Plane 33%