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    赵玉玲

    个人简历

    出生年月:1991.1

    任职年月:2021.12

    职务:    

    职称:    讲师

    所在学科:动力工程及工程热物理

    最高学位:博士/南京航空航天大学

     

    学术任职:

    1.  Physics of FluidsAerospace Science and TechnologyApplied Energy, Applied Thermal Engineering等学术期刊审稿人

    联系方式: linly-zhao@ujs.edu.cn

    研究领域

    1.       军用高温升燃烧室的燃烧性能研究,包括极端条件下点熄火特性、碳烟颗粒红外特性

    2.       民用大涵道比涡扇发动机的污染物排放控制、贫油预混燃烧振荡抑制

    3.       基于地理信息系统的全生命周期(GIS-LCA)评价

    讲授课程

    1.   航空航天工程导论

    2.   航空燃气轮机课程设计

    3.   中国航天与人文艺术(公选课)

    科研项目

    1.       江苏省基础研究计划自然科学基金青年项目(BK20240858)2024,在研,主持

    2.       江苏省高等学校自然科学研究面上项目(24KJB590001)2024,在研,主持

    3.       EEJ20涡喷发动机燃烧室研发,结题,参与

    主要论文

    1. Yuling Zhao, Mingyu Li*, Cheng Gong. Effect of mainstream-forced-entrainment control strategy on the combustion performance of a cavity-based combustor[J]. Fuel,2025,380(133265). SCI,一区, IF:6.7

    2. Jiadong Zhang, Mingyu Li, Bei Yu, Shuqi Li, Yuling Zhao*. Effect of air injection mode on the performance of a novel vortex-controlled flameholder for aircraft engine[J]. Applied Thermal Engineering,2025,262:125245.

    3. Yuling Zhao, Mingyu Li*, Tiancheng Zhou, et al. Experimental and numerical study on a cavity-swirler-based combustion strategy for advanced gas turbine engine[J]. Applied Thermal Engineering,2024,241:122470SCI,一区, IF:6.1

    4. Yuling Zhao, Jiadong Zhang, Mingyu Li*, et al. A preliminary investigation on a novel vortex-controlled flameholder for aircraft engine combustor[J]. Aerospace Science and Technology, 2024, 155:109723.

    5. Yuling Zhao, Cheng Gong, Mingyu Li*. Effect of air-injection mode on mainstream-forced entrainment and combustion characteristics of a cavity-based combustor[J]. Physics of Fluids,2024, 36:087128. SCI,一区, IF:4.1

    6. Mingyu Li, Qian Wang, Yuling Zhao*, et al. Combustion and emission characteristics of a novel staged combustor for aero gas turbine engine[J]. Aerospace Science and Technology, 2023, 134:108169.

    7. Qian Wang, Mingyu Li, Yuling Zhao*, et al. Combustion and emission performance of a trapped-vortex gas turbine combustor fueled by RP-3 kerosene[J]. FUEL, 2023,343:127929.

    8. Wu He, Yuling Zhao*, Weijun Fan. Spray, flowfield, and combustion characteristics of an external mixing atomizer in a novel cavity-swirler-based combustor[J]. Physics of Fluids,2023,35(127115) SCI,一区, IF:4.1

    9. Yuling Zhao, Xiaomin He*, et al. Ignition, efficiency and emissions of RP-3 kerosene in a three-staged multi-injection combustor[J]. Fuel Processing Technology, 2020, 213:106635.SCI,一区,IF:7.2

    10. Yuling Zhao, Xiaomin He*, et al. Effect of mainstream forced entrainment on the combustion performance of a gas turbine combustor[J]. Applied Energy, 2020,279:11584.SCI,一区, IF:10.1

    11. Yuling Zhao, Xiaomin He*, et al. Experimental investigation on spray characteristics of aircraft kerosene with an external-mixing atomizer[J]. Fuel Processing Technology, 2020,209:106531. SCI,一区, IF:7.2

    12. Yuling Zhao, Xiaomin He*, et al. Effect of cavity-air injection mode on the performance of a trapped vortex combustor[J]. Aerospace Science and Technology, 2020, 106:106183.SCI,一区, IF:5.1

    13. Mingyu Li, Xiaomin He*, Yuling Zhao, et al. Performance enhancement of a trapped-vortex combustor for gas turbine engines using a novel hybrid-atomizer[J]. Applied Energy,2018,216:286-295. SCI,一区, IF:10.1

    14. 徐熙寒,赵玉玲*,李明玉,何小民. 三级旋流流场中的点火特性研究[C].中国工程热物理学会燃烧学学术年会, 2024.

    15. 赵玉玲,何小民*,李明玉.联焰板长度对驻涡燃烧室凹腔流动特性影响的数值研究[C]. 中国航空学会第十八届燃烧与传热传质学术研讨会,2015.

    16. 赵玉玲,李明玉,张彭岗,龙琳. 基于课赛结合的“航空航天概论”课程改革与实践[J],科教导刊,2025

    获奖情况

    1. 江苏省青教赛校内选拔赛三等次,2024

    2. 第十七届全国大学生节能减排社会实践与科学竞赛三等奖(唯一指导教师),2024

    3. 江苏省诗画流体力学大赛特等奖(唯一指导教师),2023

    授权专利

    1. 赵玉玲,李明玉,一种涡控式扩压器,专利号:202311354898.8(已授权)

    2. 赵玉玲,徐熙寒,单民,卢江河,李澄阳.一种适配SAF的油气反旋空气雾化喷嘴,申请号202411521222.8

    3. 何小民,赵玉玲,等. 一种气旋耦合喷嘴,专利号:201610176845.5(已授权)

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