基本情况

教育经历

2000.9-2005.4：北航宇航学院，获航空宇航推进理论与工程专业工学博士学位

1996.9-2000.7：北航宇航学院，获飞行器动力工程（航天）专业工学学士学位

工作经历

2007.6-至 今：北航宇航学院，副教授

2007.4-2007.6：北航宇航学院，讲师

2005.4-2007.4：北航自动化科学与电气工程学院，博士后

获奖

2004、2007、2011年，北航科技进步二等奖

2011年，何鸿燊奖教金一等奖

2008年，北航优秀博士学位论文

2007年，北航"蓝天新秀"

Changhui Wang

Associate Professor

Ph.D. Beihang University (BUAA), 2005

B115, New Main Building

13426211680

wangchanghui@buaa.edu.cn

EDUCATION

Ph.D., Aerospace Propulsion Theory and Engineering, 2000.9-2005.4

School of Astronautics, BUAA

B.S., Spacecraft Power Engineering, 1996.9-2000.7

School of Astronautics, BUAA

PROFESSIONAL HISTORY

Associate Professor of Aerospace Propulsion, 2007.6- present

School of Astronautics, BUAA

Assistant Professor of Aerospace Propulsion, 2007.4- 2007.6

School of Astronautics, BUAA

Postdoctoral Researcher of Electrical Engineering, 2005.4- 2007.4

School of Automation Science and Electrical Engineering, BUAA

AWARDS and HONORS

Scientific Research Award, 2004, 2007 and 2011, BUAA

Excellent Teaching Award, 2011, He Hongshen Aerospace Science and Technology Talent Training Foundation

Best Ph.D. Dissertation Award, 2008, BUAA

Outstanding Young Teacher Award, 2007, BUAA

RESEARCH

Changhui Wang acted as principal or co-principal investigator for projects supported by the National HighTechnology Research and Development Program("863"Program) of China, the National Natural Science Foundation of China, Specialized Research Fund for the Doctoral Program of Higher Education the National Science Foundation for Post-doctoral Scientists of China and Aerospace Technology Research Fund. He has established research projects dealing with various fluid dynamic and combustion problems which arise in both solid and liquid rocket propulsion systems. His research has involved numerical analyses and experimental studies in the areas of aerospike nozzle, long-time operating solid rocket motor, multi-pulse solid rocket motor, plasma assisted combustion, low-cost high speed target missile and flow separation and side-load in rocket nozzle of large expansion ratio. He is the author or co-author of more than fifty technical papers in the areas of aerospace propulsion.

RESEARCH INTERESTS

New Technology for Solid Rocket Motor

-Long-time Operating Solid Rocket Motor

-Multi-pulse Solid Rocket Motor

-Thermal Protection and Ablation Resistance

Plasma Assisted Combustion

Plasma Characteristics of Rocket Nozzle Plume

TEACHING

Undergraduate Courses (in Chinese)

-Engineering Thermodynamics

-General Introduction to Unmanned Aerial Vehicle System

-Experimental Techniques for Rocket Engine

Graduate Courses (in Chinese)

-Advanced Rocket Propulsion

-Data Acquisition and Experiment Control for Rocket Engine Tests

Foreign Student Graduate Course (in English)

-Computational Fluid Dynamics

研究方向

固体火箭发动机

-长时间工作固体发动机

-脉冲固体发动机

-防热烧蚀

等离子体强化燃烧

发动机喷管尾焰等离子体特性

科研成果

负责和参与过国家863、国家自然科学基金、博士点基金、博士后基金、航天基金等多个项目的研究工作。主要研究固体、液体火箭发动机各种流体动力问题和燃烧问题，包括气动塞式喷管技术、长时间工作固体火箭发动机技术、脉冲固体火箭发动机技术、等离子体强化燃烧技术、低成本高速巡航靶目标技术、大面积比喷管激波分离流动等方面的理论和试验研究。发表论文50余篇。

主讲课程

本科生《工程热力学与传热学》、《无人机系统概论》、《火箭发动机综合实验》；

研究生《火箭发动机综合实验》、《火箭发动机新技术》；

留学生《Computational Fluid Dynamics》。