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李敬轩 ( 教授 ) 赞
的个人主页 http://shi.buaa.edu.cn/ljxuaa/zh_CN/index.htm
教授博士生导师硕士生导师

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[1] .Tengyu Liu, Lijun Yang, Lizi Qin, Xiaozhen Jiang, Jingxuan Li, Models of the time-averaged heat release rate of the two-dimensional laminar premixed slit flame subjected to the transverse disturbance:Aerospace Science and Technology,2023
[2] .Jiawei Wu, Jiaqi Nan, Lijun Yang, Jingxuan Li, Reconstruction of the flame nonlinear response using deep learning algorithms:Physics of Fluids,2023
[3] .Dongbin Wang, Jiaqi Nan, Lijun Yang, Aimee S Morgans, Jingxuan Li，Analytical solutions for the acoustic field in thin annular combustion chambers with linear gradients of cross-sectional area and mean temperature:Aerospace Science and Technology,2022,132
[4] .Xiaozhen Jiang, Jingxuan Li, Aimee S. Morgans, Lijun Yang,Nonlinear response of laminar premixed flames to dual-input harmonic disturbances.[C]:The 51st International Congress and Exposition on Noise Control Engineering,2022
[5] .Liang Ji, Fang Yuanqi, Jingxuan Li, Gaofeng Wang, Li-jun Yang,A 2D low-order thermoacoustic network model of annular combustor with baffles in the plenum.[C]:The 51st International Congress and Exposition on Noise Control Engineering,2022
[6] .Song Y, Liu X, Li J, et al. Effect of the flame motion on azimuthal combustion instabilities.[期刊]:Aerospace Science and Technology,2022,130(107930)
[7] .Zhu S, Liu Y, Liang X, et al. The acoustic transfer impedance of baffled injectors in three-dimensional combustion chambers.[期刊]:Aerospace Science and Technology,2022,130(107868)
[8] .Liang X, Yang L, Wang G, et al. Hopf Bifurcation Analysis of the Combustion Instability in a Liquid Rocket Engine.[期刊]:Aerospace,2022,9(10)
[9] .Gao Y, Zhang B, Cheng J, et al. Influence of Flow Rate Distribution on Combustion Instability of Hypergolic Propellant.[期刊]:Aerospace,2022,9(10)
[10] .Nan J, Li J, Yang L. Three-Dimensional Analytical Solutions for Acoustic Transverse Modes in a Cylindrical Duct with Axial Temperature Gradient and Non-Zero Mach Number.[期刊]:Aerospace,2022,9(10)

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