Characteristics of the recirculation zone downstream a dual-swirl cup at varied inlet Reynolds numbers
Investigation on a centrically slit flame holder for afterburner
The Effect of Flow Field and Fuel Spray of Combustor with Swirl Cup on Lean Blowout Limit at Idle Condition
Effect of flame stabilizer relative parameters on combustion and flow field in water ramjet
基于自适应MOMEDA滚动轴承故障特征提取方法
Related Author
YU Bo-wen
ZHANG Chi
YANG Qian
XU Quan-hong
LIN Yu-zhen
ZHANG Xiao-chun
LI Jiang-ning
XU Xing-ping
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
Shenyang Aeroengine Research Institute, China Aviation Industry Corporation Ⅰ
College of Power and Energy Engineering, Huazhong University of Science and Technology
Beijing University of Aeronautics and Astronautics
Advanced Gas Turbine Laboratory,Institute of Engineering Thermophysics,Chinese Academy of Sciences