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讲师 - 张悦
姓名: 张悦 性别
学位与职务: 博士/讲师 现任职务:
硕导/博导: 硕导 出生年月: 1986.10
学术经历:
2016.1至今 南京航空航天大学讲师
从事学科与研究方向:
主要从事进气道复杂内流机理与控制方面的基础理论与关键技术研究,具体研究方向如下:
1)内流中激波/边界层干扰的机理;
2)进气道内先进流动控制技术;
3)新概念超声速/高超声速可变形进气道;
4)粒子分离器。
学术兼职:
担任AIAA Journal of Thermophysics and Heat Transfer的审稿专家;
荣誉称号:
教学与科研情况:
目前,为能源与动力工程专业学生讲授《工程流体力学》,学时数56。
负责国家973项目专题一项,参与国家自然基金重点项目、国家重大科技工程项目等,以第一作者在AIAA Journal、Journal of Propulsion and Power等国外航空航天领域权威期刊发表SCI论文6篇,具体如下:
1.Yue Zhang, Hui-jun Tan, Fang-chao Tian and Yi Zhuang. Control of Incident Shock/Boundary Layer Interaction by a Two-Dimensional Bump,
AIAA Journal, Vol. 52, No. 4, 2014
2.Yue Zhang, Hui-jun Tan, Shu Sun and Cai-yan Rao. Control of Cowl Shock/Boundary Layer Interaction in Hypersonic Inlets by a bump, AIAA Journal, Vol. 53, No. 11, 2015
3.Yue Zhang, Hui-jun Tan, Yi Zhuang and De-peng Wang. Influence of Expansion Waves on Cowl Shock/Boundary Layer Interaction in Hypersonic Inlets, Journal of Propulsion and Power, Vol. 30, No. 5, pp. 1183-1191, 2013
4.Yue Zhang, Hui-jun Tan, Mo-chen Du and De-peng Wang. Control of Shock/Boundary Layer Interaction for Hypersonic Inlets by Highly Swept Microramps, Journal of Propulsion and Power, Vol. 31, No. 1, pp. 113-143, 2015
5.Yue Zhang, Hui-jun Tan , Yi Zhuang and De-peng Wang. A Morphing Supersonic Inlet with Special Air Cell, Journal of Propulsion and Power, Vol. 31, No. 2, pp. 583-591, 2015
6.Yue Zhang, Hui-jun Tan, Shu Sun and Hao Chen. Experimental and Numerical Investigation of a Fluidically Variable Hypersonic Inlet, AIAA Journal, acceptted, 2017

联系方式:
邮箱:y.zhang@nuaa.edu.cn
手机:15950519032