Flame response to acoustic excitation in a rectangular rocket combustor with LOx/H 2 propellants

Keyphrases

• Propellant 100%
• Flame Response 100%
• Acoustic Excitation 100%
• Rocket Combustor 100%
• Combustor 66%
• Acoustic Forcing 66%
• Combustion Chamber Pressure 66%
• Combustion Chamber 33%
• Aerospace 33%
• Emission Intensity 33%
• Oscillation 33%
• Deflection 33%
• Resonant Mode 33%
• Pressure Condition 33%
• Injection Condition 33%
• Self-sustaining 33%
• Hydroxyl Radical 33%
• Excitation Frequency 33%
• Overpressure 33%
• OH* Chemiluminescence 33%
• OH Emission 33%
• Forced Excitation 33%
• Optical Access 33%
• Chemiluminescence Imaging 33%
• Rocket Engine 33%
• Combustion Instability 33%
• Potential Indicators 33%
• Acoustic Resonance 33%
• High Frequency Combustion Instability 33%

Engineering

• Combustor 100%
• Combustion Chamber 100%
• Chamber Pressure 66%
• Resonance Mode 33%
• Emission Intensity 33%
• Excitation Frequency 33%
• Rocket Engine 33%
• Chemiluminescence Imaging 33%
• Acoustic Resonance 33%