a foreground configuration system and background operating system were designed to establish the aero-engine configuration modeling platform.Steady and transient simulations of variable kinds of aero-engines were successfully conducted on the platform.The results of good precision verify the feasibility for aero-engine configuration modeling technology.
High speed solenoid valve with the application of AMESim
Development path and future trend of carrier-based advanced trainer engine
Thermal protection effectiveness of thermal barrier coatings in turbine blade applications
Aero-engine cycle design approach for multiple operating conditions performance reliability
Relationship between rotor/vanes blade number andnodal diameter number of bladed-disk coupling vibration
Related Author
WANG Qiu-xia
FAN Ding
PENG Kai
PENG Yunlong
WU Xiong
DING Ting
ZHU Jianqin
ZHAO Chaofan
Related Institution
School of Power and Energy,Northwestern Polytechnical University
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics