Effect of Fuel Reactivity and Operating Conditions on Flame Anchoring in the Premixing Zone of a Swirl Stabilized Gas Turbine Combustor

Keyphrases

• Flame Anchoring 100%
• Operating Conditions 100%
• Gas Turbine Combustor 100%
• Premixed 100%
• Swirl-stabilized 100%
• Fuel Reactivity 100%
• Preheating Temperature 33%
• Lean Premixed 22%
• Global Equivalence Ratio 22%
• Flame Stabilization 11%
• Laser Pulse 11%
• High-speed Imaging 11%
• Atmospheric Pressure 11%
• Mass Fraction 11%
• Inherent Risk 11%
• Tent 11%
• Steady Operation 11%
• Burner 11%
• Operating Parameters 11%
• Air-fuel Mixture 11%
• Flame Characteristics 11%
• OH* Chemiluminescence 11%
• Characteristic Timescales 11%
• Combustion Characteristics 11%
• Flashback 11%
• Premixed Gas 11%
• Air Mass Flow Rate 11%
• Swirl-stabilized Burner 11%
• Characteristic Comparison 11%
• Damköhler 11%
• Hydrogen-blended Natural Gas 11%

Engineering

• Gas Turbine Combustors 100%
• Preheat Temperature 100%
• Equivalence Ratio 66%
• Experimental Investigation 33%
• Characteristic Time 33%
• Natural Gas 33%
• Mass Flowrate 33%
• Operating Parameter 33%
• Mass Fraction 33%
• Atmospheric Pressure 33%
• Gas Mixture 33%
• Air Mass 33%