Numerical simulation of the effects of pulsed injection on combustion and flow processes in a supersonic combustor

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作者
He, Zan [1 ]
Tian, Ye [1 ,2 ]
Le, Jialing [1 ,2 ]
机构
[1] School of Power and Energy, Northwestern Polytechnical University, Shanxi, Xi'an,710072, China
[2] Key Laboratory of Cross-Domain Flight Interdisciplinary Technology, China Aerodynamic Research and Development Center, Sichuan, Mianyang,621000, China
关键词
Combustors - Hydrogen engines - Ignition - Navier Stokes equations - Oscillating flow;
D O I
10.1063/5.0234223
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