Aviation Aerospace Promotion Theory and Engineering

Basic Cases

National Key Discipline (Aviation Aerospace Science and Technology): Beijing University of Aeronautics and Astronautics, Northwestern University of Technology, Nanjing University of Aeronautics University

National Key Discipline ( Aviation Aerospace Promotion Theory and Project): China People's Liberation Army University of Defense Technology, China People's Liberation Army Air Force Engineering University

Research Direction

"Aviation Aerospace Promotion Theory and Engineering" Secondary Discipline includes aviation Engines and rocket engines.

"doctoral" cultivation direction

1. Overall optimization and computer-aided design

includes propulsion theory and propulsion plan; propulsion system integrated design and parallel engineering design; overall performance parameter optimization design; structural optimization design and computer aided design; engine work process simulation; Promoting system usage performance, etc.

2. Inner flow field and pneumatic mechanics, pneumatic acoustic

including engine internal flow field calculation and experimental research; impeller aerodynamics, pneumatic elastic mechanics and pneumatic acoustic acoustic; impeller non-fixed flow theory, experiment and application; engine Pneumatic thermodynamics of intake, combustion chamber and exhaust system.

3. Combustion and Combustion Chamber

contain combustion indoor spray, blending and combustion; numerical simulation and experimental study of combustion process; combustion pollution control, etc.

4. Transfer and mass transfer

containing heat, mass transfer and thermal protection theory and application; numerical simulation and experimental study of heat transfer, mass transfer.

5. Strength, vibration, reliability and maintenance

Containing long-term temperature prediction and component damage tolerance design; structural system vibration analysis and vibration control technology; high speed rotor dynamics; structural system reliability analysis With design, etc..

6. Engine control, test, status monitoring and troubleshooting

contains aircraft / propulsion system digital electronic comprehensive control; promoting system modeling, control and simulation; advanced system of promoting system; advancement of system monitoring Diagnostic technology, etc.

7. Rocket Engine Design and Working Process Simulation

including solid rocket engine, liquid rocket engine and special rocket engine design and work process simulation, involving flow field, heat transfer, strength, system characteristics, rotor kinetics, optimization design , Engine performance, etc.

8. Rocket Engine New Technology and New Rocket Engine

Includes a new generation of solid rocket engines, liquid rocket engines key technologies, electromagnetic promotion techniques, nuclear promotion techniques, and stamping engine technology.

9. Rocket Engine Test and Advanced Measurement Technology

include test and measurement techniques of solid rocket engines and liquid rocket engines, and research on new ignition techniques, spray combustion techniques, and turbine pump technology.