Experimental study on transition between ramjet and scramjet modes in a dual-mode combustor

Keyphrases

• Combustor 100%
• Strut 100%
• Dual-mode Combustor 100%
• Ramjet Mode 100%
• Scramjet Mode 100%
• Injection Pressure 66%
• Combustion 66%
• Pilot Flame 66%
• Combustion Chamber 33%
• Pressure Peak 33%
• Challenging Tasks 33%
• Mach number 33%
• Air-breathing 33%
• Propulsion 33%
• Methane 33%
• Injector 33%
• Flame Holder 33%
• Launcher 33%
• System Integration 33%
• Dual-mode 33%
• Cylindrical pipe 33%
• Blockage 33%
• Aerodynamics 33%
• Take-off 33%
• Combustion Process 33%
• Pressure Interval 33%
• Schlieren Imaging 33%
• Premixed 33%
• Constant Cross-section 33%
• Recirculation Area 33%
• Static Pressure 33%
• Hypersonic Flight 33%
• Injection System 33%
• Propulsion Unit 33%
• Air-breathing Electric Propulsion 33%
• Wall Static Pressure 33%
• Dual-fuel Combustion 33%
• Static Pressure Measurement 33%
• Total Temperature 33%
• Strut Injector 33%
• Future Solutions 33%
• Supersonic Airflow 33%
• Air-breathing Engine 33%
• Flow Recirculation 33%

Physics

• Supersonic Combustion Ramjet Engine 100%
• Static Pressure 100%
• Combustion Chamber 50%
• Pressure Measurement 50%
• Methane 50%
• Spacecraft 50%
• Flame Holder 50%
• Supersonics 50%
• Mach Number 50%
• Air Flow 50%
• Hypersonic Flight 50%
• Takeoff 50%
• Combustion 50%

Engineering

• Combustor 100%
• Injection Pressure 50%
• Breathing 50%
• Mach Number 25%
• Combustion 25%
• Schlieren 25%
• Broad Range 25%
• Mode Operation 25%
• Takeoff 25%
• Combustion Mode 25%
• Cross-Section Constant 25%
• Injection System 25%
• Air Breathing Propulsion 25%
• Static Pressure Measurement 25%
• Static Pressure 25%
• Methane 25%
• Air Flow 25%
• Combustion Chamber 25%