the individual droplet burning behavior was added into the traditional point source two phase turbulent combustion model (TM)
and then a full status two phase turbulent combustion model (FSM) was presented.The two kinds of two phase turbulent combustion models were tested by a set of methanol air two phase turbulent spray jet flame experimental data.The comparison results between the computational prediction results and the experimental data show that the FSM model can give two peaks in the averaged temperature profile
Large eddy simulation of cryogenic jet under supercritical pressure based on OpenFOAM
Analysis of n⁃dodecane spray jet by proper orthogonal decomposition
Experimental research progress in combustion of metal under microgravity
Large eddy simulation on the staggered tube bundle of the compact precooler
Study on opposed mixing flow in circumferential intake
Related Author
Yuhang LI
Baoyuan WU
Yi WANG
Lixin ZHOU
Wenjin QIN
Lihui XU
Dengbiao LU
Hao LIU
Related Institution
National Key Laboratory of Science and Technology on Liquid Rocket Engines,Xi'an Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation
Academy of Aerospace Propulsion Technology,China Aerospace Science and Technology Corporation
School of Mechanical Engineering, University of Shanghai for Science and Technology
Beijing Aerospace Institute for Metrology and Measurement Technology, China Academy of Launch Vehicle Technology, China Aerospace Science and Technology Corporation
Institute for Thermal Power Engineering, Zhejiang University