Combustion instabilities of ultra-lean premixed H₂∕Air mixtures by prechamber turbulent jet ignition

Keyphrases

• Combustion Instability 100%
• Pre-chamber 100%
• Lean Premixed 100%
• Ultra-lean 100%
• Turbulent Jet Ignition 100%
• Equivalence Ratio 66%
• Turbulent Jet 66%
• Instability Mode 66%
• Main Chamber 66%
• Heavy-duty 33%
• Mixed Mode 33%
• Combustor 33%
• Strong Coupling 33%
• Strain Measurement 33%
• Strain Rate 33%
• Response Model 33%
• Phaseless Measurements 33%
• Heat Release 33%
• Pressure Field 33%
• Ignition 33%
• Pressure Spectrum 33%
• Acoustic Disturbance 33%
• Dual-chamber 33%
• Field Perturbation 33%
• Lean Burn 33%
• Physical Significance 33%
• Transverse Mode 33%
• Lean Conditions 33%
• Dynamic Mode Decomposition 33%
• Primary Instability 33%
• Thermoacoustics 33%
• Longitudinal Mode 33%
• Pressure Perturbation 33%
• Acoustic Resonator 33%
• Schlieren 33%
• Flame Propagation 33%
• Unstable Combustion 33%
• Combustion Response 33%
• Linearized Euler Equations 33%
• Gas Engine 33%
• Lean Flame 33%
• OH* Chemiluminescence 33%
• Unstable Flame 33%
• Pre-chamber Jet Ignition 33%
• Pre-chamber Combustion 33%
• Thermoacoustic Instability 33%
• Modeling Results 33%
• Flame Edges 33%

Engineering

• Ignition 100%
• Equivalence Ratio 66%
• Instability Mode 66%
• Main Chamber 66%
• Schlieren 33%
• Rates of Strain 33%
• Combustor 33%
• Resonator 33%
• Mixed Mode 33%
• Mode Dynamic 33%
• Model Response 33%
• Frequency Domain 33%
• Heat Release 33%
• Longitudinal Mode 33%
• Pressure Perturbation 33%
• Physical Significance 33%
• Linearized Euler Equation 33%
• Thermoacoustic Instability 33%
• Flame Propagation 33%
• Pressure Distribution 33%
• Gas Engine 33%