A5076528223- Refrigeration and Air Conditioning Technologies
- Heat transfer and supercritical fluids
- Computational Fluid Dynamics and Aerodynamics
- Fluid Dynamics and Turbulent Flows
- Heat Transfer and Optimization
- Advanced Combustion Engine Technologies
- Advanced Thermodynamic Systems and Engines
- Subcritical and Supercritical Water Processes
- Phase Equilibria and Thermodynamics
- Thermodynamic and Exergetic Analyses of Power and Cooling Systems
- Advanced Sensor Technologies Research
- Heat Transfer Mechanisms
- Hydraulic and Pneumatic Systems
- Plasma and Flow Control in Aerodynamics
- Rocket and propulsion systems research
- Thermochemical Biomass Conversion Processes
- Combustion and flame dynamics
- Gas Dynamics and Kinetic Theory
- Spacecraft and Cryogenic Technologies
- Turbomachinery Performance and Optimization
- Aerodynamics and Fluid Dynamics Research
- Advancements in Solid Oxide Fuel Cells
- Nuclear reactor physics and engineering
- Combustion and Detonation Processes
- Heat Transfer and Boiling Studies
Tsinghua University
2016-2025
Xi'an Jiaotong University
2005-2023
Hubei Normal University
2023
Xiangtan University
2012
Nanyang Technological University
2007-2008
Hypersonic vehicles with turbojet, ramjet, and scramjet engines are expected to be widely applied future transportation systems. Due high-speed flight in the atmosphere, body outer surfaces suffer strong aerodynamic heating, on other hand, combustion chamber inter walls under extremely high temperature heat flux. Therefore, more efficient stable active cooling technologies required hypersonic vehicles, such as regenerative cooling, film transpiration well their combinations. This paper...
The flow and heat-transfer behavior of thermal cracking n-decane was investigated experimentally numerically. An electrically heated vertical tube (2 mm inner diameter) applied to carry out supercritical pressure at various pressures, temperatures, resident times. results showed that the second-order reactions increase formation rates light products (especially CH4 C2H4) for conversions greater than 13%, while heavy product (C5–C9) are decreased. A global reaction model is given less...
Regenerative cooling is being used to meet the high requirements of advanced hypersonic flight vehicles using fuel at supercritical pressures as coolant. The heat transfer and thermal cracking characteristics vary with pressure, mass flow rate flux. This work presents an experimental investigation pressure hydrocarbon fuels their interactions. A proportional production distribution chemical model was developed for pre-exponential factor activation energy describe reactions. Numerical results...