Investigation on the stability of the Rijke-type thermoacoustic system with an axially distributed heat source

Engineering

• Acoustic Energy 100%
• Aero-Engines 50%
• Combustor 50%
• Dynamic Behavior 50%
• Energy Gain 50%
• Experimental Work 50%
• Flow Field 50%
• Flow Velocity 100%
• Heat Source 100%
• Non-Linear Dynamic 50%
• Numerical Methods 50%
• Phase Difference 50%
• Propulsion System 50%
• Rijke Tube 50%
• Rocket Engine 50%
• Thermoacoustic Instability 50%
• Vortex 50%

Physics

• Acoustic Coupling 14%
• Combustion Chamber 14%
• Cross Correlation 14%
• Flow Distribution 14%
• Flow Velocity 28%
• Heat Sources 100%
• Mathematical Method 14%
• Non-Linear Dynamic 14%
• Rocket Engine 14%
• Thermoacoustics 100%