A NUMERICAL METHOD FOR PREDICTING TURBINE PROFILE LOSS
Effects of loading distribution on a vaned diffuser
Influence of suction-side winglet length on tip leakage flow in compressor cascade
Numerical simulation and hot test investigation of plug nozzle in solid rocket motor
Analysis of characteristic and mechanism of pipe diffuser for a highly loaded centrifugal compressor
Related Author
Yu Qing
Yang Hong
CAO Si
LIU Bao-jie
HAN Shao-bing
ZHONG Jing-jun
YAN Hong-ming
REN Jun-xue
Related Institution
th Dept.Beijing University of Aeronautics and Astronautics
th Dept. Harbin Institute of Technology
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
School of Energy Science and Engineering, Harbin Institute of Technology
Marine Engineering College, Dalian Maritime University