Combustion instabilities in a bifurcating tube: Open- and closed-loop measurements

Engineering

• Closed Loop 100%
• Open Loop 100%
• Flow Field 66%
• Sound Pressure Level 66%
• Acoustic Field 66%
• Experimental Result 33%
• Computer Simulation 33%
• Good Agreement 33%
• Gas Turbine 33%
• Mode Shape 33%
• Flow Rate 33%
• Two Dimensional 33%
• Input Multi 33%
• Fuel Flow 33%
• Experimental Measurement 33%
• Aeroengine 33%
• Loop Control System 33%
• Combustion System 33%
• Single Output 33%
• Pressure Sensor 33%
• Function Analysis 33%
• Open End 33%
• Limit Cycle 33%
• Oscillating Flow 33%
• Cycle Frequency 33%
• Sustained Oscillation 33%

Physics

• Fuel Flow 25%