Topology optimization of regenerative cooling channel in non-uniform thermal environment of hypersonic engine

Engineering

• Cooling Channel 100%
• Thermal Environment 100%
• Fossil Fuel 33%
• Design Optimization 16%
• Pressure Drop 16%
• Flow Distribution 16%
• Temperature Distribution 16%
• Microchannel 16%
• Pyrolysis 16%
• Thermal Protection 16%
• Flow Phenomenon 16%
• Nonuniformity 16%
• Local Heat Transfer 16%
• Adverse Pressure Gradient 16%
• Cooling Capacity 16%
• Temperature Region 16%
• System Protection 16%
• Reverse Flow 16%
• Heated Wall 16%
• Uniform Heat Flux 16%
• Supercritical Flow 16%
• Active Cooling 16%
• Heat Transfer Phenomenon 16%