EXPERIMENTAL INVESTIGATION OF HIGH FREQUENCY FLAME RESPONSE ON INJECTOR COUPLING IN A PERFECTLY PREMIXED MULTI-JET COMBUSTOR

Keyphrases

• Acoustic Coupling 14%
• Acoustic Pressure Fluctuation 14%
• Acoustic Velocity 28%
• Acoustics 14%
• Antinode 14%
• Coherent Vortex Structures 14%
• Combustion Chamber 14%
• Combustor 100%
• Deformation Displacement 14%
• Delay Model 14%
• Displacement Mechanism 14%
• Feed Flow 14%
• Feedback Mechanism 28%
• Flame Deformation 14%
• Flame Displacement 14%
• Flame Response 100%
• Flow Modulation 14%
• Full Period 14%
• Gas Turbine Engine 14%
• Heat Release 14%
• Heat Release Fluctuation 14%
• High-frequency Instability 14%
• Injector 100%
• Local Fluctuations 14%
• Multi-jet 100%
• Node Coupling 14%
• Numerical Simulation 14%
• Oscillation 14%
• Phase Locking 14%
• Premixed 100%
• Rayleigh Integral 14%
• Rocket 14%
• Thermoacoustic Instability 28%
• Thermoacoustics 42%
• Three-dimensional (3D) 14%
• Tube Length 14%
• Wave number 14%

Engineering

• Acoustic Pressure 25%
• Antinode 25%
• Combustion Chamber 75%
• Combustor 100%
• Convective 25%
• Delay Time 25%
• Experimental Investigation 100%
• Experimental Result 25%
• Feedback Mechanism 50%
• Gas Turbine Engine 25%
• Heat Release 50%
• Main Source 25%
• Nodes 25%
• Pressure Fluctuation 25%
• Similarities 25%
• Thermoacoustic Instability 50%
• Vortex 25%
• Wave Number 25%