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

Physics

• Acoustic Excitation 33%
• Acoustic Resonance 16%
• Acoustics 33%
• Combustion Chamber 100%
• Combustion Stability 33%
• Cryogenics 16%
• Deflection 16%
• Flames 50%
• Frequencies 16%
• High Speed 16%
• Hydrogen 16%
• Injection 16%
• Oscillation 16%
• Oxygen 16%
• Pressure 16%
• Propellant 50%
• Responses 50%
• Running 16%
• Utilization 16%
• Variations 16%

Engineering

• Acoustic Resonance 16%
• Acoustics 33%
• Applications 16%
• Chamber Pressure 33%
• Chemiluminescence Imaging 16%
• Combustion Chamber 50%
• Combustor 50%
• Emission Intensity 16%
• Excitation Frequency 16%
• Flame 50%
• High Frequency 16%
• High Speed 16%
• Mechanisms 33%
• Research 16%
• Resonance Mode 16%
• Rocket Engine 33%
• Testing 16%