Experimental study on thermal load characteristics of a U-bend pulse detonation combustor

Engineering

• Combustor 100%
• Thermal Load 100%
• Turbine 66%
• Heat Flux 33%
• External Wall 33%
• Detonation Wave 16%
• Temperature Range 16%
• Temperature Increase 16%
• Constant Value 16%
• Flow Direction 16%
• Heat Loss 16%
• Energy Dissipation 16%
• Pressure Gain Combustion 16%
• Thermal Equilibrium 16%