西安交通大学航天航空学院导师教师师资介绍简介-左逢源

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基本信息 - 左逢源基本信息

左逢源，讲师，硕士生导师
博士后创新人才支持计划
陕西省高校科协青年人才托举

联系方式

电邮：fengyuan@xjtu.edu.cn
西安交通大学兴庆校区航天学院东417
中国西部科技创新港，力行楼，2-4095

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个人简介

主持国家自然基金青年项目，博士后创新人才支持计划（航空宇航口），陕西省高校科协青年人才托举计划，博士后面上基金等项目。以第一作者在Prog. Aerosp. Sci.、J. Fluid Mech.、AIAA J. 等期刊发表多篇SCI论文。受Prof. M. Platzer主编邀稿，介绍了冲压进气道近70年的发展历程，以综述的形式发表在航空顶刊Progress in AerospaceSciences. 另一篇选为期刊封面，发表在流体力学顶刊Journal ofFluid Mechanics。担任J. Fluid Mech.审稿人。
工作于西交大航天学院申胜平教授团队，并与Sapienza University of Rome, Ryerson University的航空知名教授Prof. Sergio, Prof. Sannu保持长期合作交流，每年可招收硕士生，欢迎对航空航天感兴趣的同学们加入团队！

研究领域
高超声速推进系统设计；激波/边界层干扰；飞行器/进气道一体化设计;

科研项目

国家自然基金青年项目，**, 2021.1-2023.12, 24万, 纵向, 主持
博士后创新人才支持计划，BX**, 2020-2022, 63万, 纵向, 主持
陕西省高校科协青年人才托举计划，**, 2021.1-2022.12, 纵向, 主持
中央高校基本科研业务费，xzy, 2020.1-2022.12, 纵向, 主持
博士后面上基金，2020M673411, 2020-2022, 8万, 纵向, 主持
XXX流动控制技术，**, 2021.3-2021.12, 横向, 主持

教育及工作经历
2019.12-至今, 西安交通大学讲师
2017.11-2018.11, Sapienza University of Roma
航空宇航推进理论与工程，联合培养博士
2013.09-2019.09, 南京航空航天大学
航空宇航推进理论与工程，博士(直博)
2009.09-2013.06, 南京航空航天大学
飞行器动力工程专业，学士

学术论文 - 左逢源学术论文

* 代表通讯作者
Fengyuan Zuo*. The scaling of separation bubble in the conical shock wave/turbulent boundary layer interaction.Acta Astronautica. 2021, 186: 418-425.
左逢源*. 内转式TBCC组合动力进气道设计方法研究进展. 清华大学学报(自然科学版)，2021，已录用.
Fengyuan Zuo*, Shuling Hu. Thermochemical non-equilibrium effects on aerothermodynamic prediction of laminar double-cone flow. Acta Astronautica. 2021, 182: 179-188.
Fengyuan Zuo*, Antonio Memmolo, Sergio Pirozzoli. Reynolds-averaged numerical simulations of conical shock wave/boundary layer interactions. AIAA Journal. 2021, 59(5): 1645–1659.
Fengyuan Zuo*, Sannu M?lder, Gang Chen. Performance of wavecatcher intakes at angles of attack and sideslip. Chinese Journal of Aeronautics. 2021, 34(7): 244-256.
Fengyuan Zuo*, Antonio Memmolo. Investigation of conical shock wave/boundary layer interaction in axisymmetric internal flow. Aerospace Science and Technology. 2020, 106: 106106.
Fengyuan Zuo*, Antonio Memmolo, GuopingHuang, Sergio Pirozzoli**. Direct numerical simulation of conical shock wave-turbulent boundary layer interaction. Journal of Fluid Mechanics. 2019, 877: 167-195.(Featured on cover)
Fengyuan Zuo*, Sannu M?lder. Hypersonic wavecatcher intakes and variable-geometry turbine based combined cycle engines. Progress in Aerospace Sciences. 2019, 106: 108-144.(邀稿综述)
Fengyuan Zuo*,GuopingHuang. Numerical investigation of bleeding control method on section-controllable wavecatcher intakes. Acta Astronautica. 2018, 151: 572-584.
Fengyuan Zuo*,GuopingHuang, Chen Xia. Investigation of internal-waverider-inlet flow pattern integrated with variable-geometry for TBCC. Aerospace Science and Technology. 2016, 59: 69-77.
Fengyuan Zuo*, Guoping Huang, Chen Xia. Bleeding control for improving internal waverider inlet self-starting ability. International Journal of Turbo & Jet-Engines. 2019, 36(1): 51-60.
Guoping Huang,Fengyuan Zuo*, Wenyou Qiao. Design method of internal waverider inlet under non-uniform upstream for inlet/forebody integration. Aerospace Science and Technology. 2018, 74: 160-172.
左逢源,黄国平,陈杰,唐伟员.基于内乘波概念的TBCC进气道过渡模态研究.工程热物理学报, 2015, 36(2): 274-278.
国际会议
Fengyuan Zuo*,GuopingHuang, Chen Xia, WeiyuanTang. Investigation of the self-starting ability of an internal waverider inlet for ramjet. 51st AIAA Joint Propulsion Conference.Orlando, FL, United States: AIAA Paper 2015-3748, 2015.
Fengyuan Zuo*,GuopingHuang, HuihuiHuang, Chen Xia. Analyzing the parent flowfield of inward turning inlet combined with variable-geometry. 52nd AIAA Joint Propulsion Conference.Salt Lake City, UT, United States: AIAA Paper 2016-4574, 2016.
Fengyuan Zuo*,GuopingHuang. A preliminary overview analysis on the internal waverider inlets for ramjet. 21st AIAA International Space Planes and Hypersonics Technologies Conference.Xiamen, China: AIAA Paper 2017-2420, 2017.
Guoping Huang, Fengyuan Zuo*, Wenyou Qiao, Chen Xia. Design method of internal waverider inlet with bump compression surface. 53rd AIAA Joint Propulsion Conference. Atlanta, Georgia, United States: AIAA Paper 2017-4654, 2017.
Huihui Huang, Guoping Huang, Fengyuan Zuo, Chen Xia. Research on a novel internal waverider TBCC inlet for ramjet mode. 52nd AIAA Joint Propulsion Conference, 2016. Salt Lake City, UT, United States: AIAA Paper 2016-4575, 2016.
Huihui Huang, Guoping Huang, Fengyuan Zuo, Chen Xia. CFD simulation of TBCC inlet based on internal waverider concept. 21st AIAA International Space Planes and Hypersonics Technologies Conference. Xiamen, China: AIAA Paper 2017-2354, 2017.
Yongbing Pu, Guoping Huang, Fengyuan Zuo, Chen Xia. Numerical investigation of two-dimensional supersonic variable-geometry inlet for ramjet. 21st AIAA International Space Planes and Hypersonics Technologies Conference. Xiamen, China: AIAA Paper 2017-2415, 2017.

教学工作 - 左逢源讲授课程
研究生课程：
高超声速飞行器/推进系统一体化设计 32学时