Secondary flow analysis for non-axisymmetric endwall on the high-load compressor cascade
Experimental study of flow friction characteristics for a rotor-stator system with centre inflow of cooling air
端壁倒圆对低展弦比超高负荷大折转动叶端区二次流损失影响
端壁自适应射流出口位置对高速扩压叶栅角区分离的影响
基于粒子群的排气蜗壳气动和声学优化
Related Author
ZHU Jun-qiang
LU Xin-gen
WU Ji-chang
XU Guo-qiang
LUO Xiang
LI Fu-qing
赵庆军
裴吉
Related Institution
Graduate University of Chinese Academy of Sciences
Institute of Engineering Thermophysics, Chinese Academy of Sciences
National Key Laboratory of Science and Technology on Aero-Engines Aero-thermodynamics, School of Jet Propulsion,Beijing University or Aeronautics and Astronautics