The Interior Heat Transfer Characteristics of Gas Turbine Blade Due to Sparse Film Cooling Holes
Aerodynamic performance optimization onanalysis code of multi-stage axial compressor
Analysis of inlet pre-swirl influence on aerodynamic performance in highly loaded transonic fan
Numerical simulation and analysis on aerodynamics of three-element airfoil in ground effect
ICT assisted detection for remainders in the internal cooling channel of the turbine blade
Related Author
ZHANG Jing yu
CHANG Hai ping
GUO Yi
DU Gang
CHEN Jiang
YIN Hong-shun
ZHAO Bin
LIU Bao-jie
Related Institution
Nanjing University of Aeronautics and Astronautics
School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
China Gas Turbine Establishment, Aviation Industry Corporation of China
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
School of Aeronautics Science and Technology, Beijing University of Aeronautics and Astronautics