Su Wei-Yi
Associate Professor
Supervisor of Master's Candidates
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Zhang jun-xin.Reduced-order modeling of hypersonic inlet flowfield based on autoencoder and proper orthogonal decomposition.Journal of Spacecraft and Rockets.2024,online
Su Wei-Yi.基于伴随方法的冲压发动机进气道反设计研究.机械制造与自动化.2020
Su Wei-Yi.侧偏捕获对内收缩进气道起动的影响.固体火箭技术.2018
Su Wei-Yi.Transient Analysis for Hypersonic Inlet Accelerative Restarting Process.JOURNAL OF SPACECRAFT AND ROCKETS.2017
Su Wei-Yi.Control of pseudo-shock oscillation in scramjet inlet-isolator using periodical excitation.ACTA ASTRONAUTICA.2018
Su Wei-Yi.基于内锥和中心体表面流动参数分布的轴对称基准流场反设计.推进技术.2017
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飞机与发动机一体化引论
Research Projects
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动态反压作用下激波串振荡机理及其周期性射流相位控制研究, 2016/01/01-2019/12/31
可调进气道/预冷器多尺度流动换热机理及匹配设计方法研究, 2020/01/01
飞行历程下冲压**进气道激波、分离涡运动演化的快速预测方法研究, 2021/01/01-2021/10/21
高超声速进气道非线性失稳与迟滞电磁流动控制, 2011/10/08-2014/12/31
等离子体调控超声速进气道方法研究-2021/08/07
飞-发一体化试验智能设计研究, 2021/01/01
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