To investigate the mode transition in the dual mode combustor
using the method of computational fluid dynamics(CFD)
numerical simulation of hydrogen-fueled combustor flow field was conducted at different equivalence ratios
flying Mach numbers and fuel injection modes.The simulation results are found to agree well with the experimental data.Results show that increase of equivalence ratio and reduction of flying Mach number along with two-sides injection make the combustor tend to work in sub-combustion mode.
Effects of loading distribution on a vaned diffuser
Influence of suction-side winglet length on tip leakage flow in compressor cascade
Analysis of characteristic and mechanism of pipe diffuser for a highly loaded centrifugal compressor
Numerical simulation and hot test investigation of plug nozzle in solid rocket motor
Progress of investigation on combustion instability of solid rocket motors
Related Author
CAO Si
LIU Bao-jie
HAN Shao-bing
ZHONG Jing-jun
YAN Hong-ming
WANG Yi
ZHAO Sheng-feng
LU Xin-gen
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
Marine Engineering College, Dalian Maritime University
School of Energy Science and Engineering, Harbin Institute of Technology
Institute of Engineering Thermophysics, Chinese Academy of Sciences
Graduate University of Chinese Academy of Sciences