Prof. Hongchu Chen | 陈鸿初教授
Zhejiang University, China | 浙江大学
百人计划研究员
陈鸿初，浙江浦江人，1989年8月出生。浙江大学航空航天学院百人计划研究员，博士生导师。主要从事高超声速飞行器气动热辨识、导热反问题、先进热工测量等领域的研究。在航空航天和传热学核心期刊 AIAA Journal of Thermophysics and Heat Transfer, International Journal of Heat and Mass Transfer, Numerical Heat Transfer, Applied Mathematical Modelling 等期刊发表论文十余篇。在美国田纳西大学期间参与美国国家航空航天局（NASA）用埋在隔热瓦内部的热传感器反演辨识热防护系统表面温度和热流密度的项目；深入研究用导热反问题方法反演辨识高超声速气动热的新的解析和数值方法，并开展验证实验。研究了多种热防护材料的热物性和表面的气动热，如碳碳复合材料、氧化锆、硼化锆等。担任 International Journal of Heat and Mass Transfer, International Journal of Thermal Sciences, AIAA Journal of Thermophysics and Heat Transfer, Inverse Problems in Science and Engineering, Applied Mathematical Modelling, International Journal of Computer Mathematics, Annals of Nuclear Energy 等重要国际期刊的审稿人。
Title of Speech: Hypersonic Aerodynamic Heat Prediction by Solving Inverse Heat Conduction Problems
Assoc. Prof. Xuhui Li | 李旭晖副教授
Harbing Engineering University, China | 哈尔滨工程大学
Li Xuhui is an associate professor. In 2016, he received a doctor's degree from Kyushu University, one of the seven Imperial Universities in Japan. At present, he is mainly engaged in the research work of computational fluid dynamics in ship and ocean engineering, mainly involving the theory, algorithm, parallel computing of lattice Boltzmann method and finite volume method and their applications in the free-surface flow, cavitation. Relevant research achievements have been published on international mainstream journals in the field of statistical mechanics and computational fluid dynamics, such as Physical Review E, Computers and Fluids, International Journal of Heat and Mass Transfer, Philosophical Transactions A, etc. The conference report was awarded the Solid state Drive Prize at the 25th International Conference on Discrete Numerical Methods (DSFD). He was selected into the 2019 "Guangdong Province Overseas Youth Postdoctoral Introduction Project" (the original "the Pearl River Talent Plan" overseas youth talent introduction postdoctoral funding project). At present, he is devoted to developing "LiBraS", a next-generation CFD solver based on LBM that can simulate the scale of one billion to ten billion grid on GPU cluster/CPU cluster.
Dr. Zhaolin Chen | 陈肇麟博士
Nanjing University of Aeronautics and Astronautics, China | 南京航空航天大学
Dr. Zhaolin Chen obtained both his MEng (Aerospace Engineering) in 2009 and his Ph.D (Aerodynamics) in 2014 from the University of Sheffield, UK. He started his carrier working as a Post-Doctoral Research Associate at the University of Sheffield after his Pd.D under Professor Ning Qin. From 2015 to 2018, he served as a Senior Engineer in the Turbomachinery Design Department at FlaktGroup Ltd. in the United Kingdom. In 2019, He joined in the department of aircraft design of NanJing University of Aeronautics and Astronautics (NUAA). Research wise, his field of study focuses on the development of computational methods for solving governing fluid flow equations as well as optimization techniques. Specific research areas encompass steady and unsteady flow simulation solutions, mesh deformation techniques, optimization methodologies, and aerodynamic-structural coupling. Specific applications encompass aerodynamic and aeroacoustic simulation as well as optimization of wings and rotor blades. Recent efforts have concentrated on the design of aerial vehicles for Mars exploration. This includes the development of multi-fidelity codes for rotor design, aero-structural optimization of rotors, and performing experimental tests simulating the Martian environment.