Computation of transfer matrices for gas turbine combustors including acoustics/flame interaction

Keyphrases

• Acoustics 100%
• Transfer Matrix 100%
• Gas Turbine Combustor 100%
• Flame Interaction 100%
• Combustor 60%
• Four-pole Parameter 40%
• Numerical Simulation 20%
• Noisy Environment 20%
• Source Term 20%
• Experimental Determination 20%
• Traveling Wave 20%
• Heat of Reaction 20%
• Finite Element Code 20%
• Burner 20%
• Velocity Fluctuation 20%
• Combustion Instability 20%
• Reaction Zone 20%
• Combustion System 20%
• Heat Release 20%
• Experimental Field 20%
• Swirl Burner 20%
• Acoustic Transfer 20%
• Acoustic Quantities 20%
• Exit Velocity 20%
• Multi-microphone 20%

Engineering

• Combustor 100%
• Gas Turbine Combustors 100%
• Frequency Domain 50%
• Noisy Environment 50%
• Experimental Determination 50%
• Source Term 50%
• Reaction Zone 50%
• Heat Release 50%
• Velocity Fluctuation 50%
• Swirl Burner 50%
• Exit Velocity 50%
• Finite Element Analysis 50%
• Traveling Wave 50%
• Combustion Chamber 50%