基本情况

1990--1994 北航宇航学院火箭发动机专业学士

1994--1997 北航宇航学院火箭发动机专业硕士

1997--2000 北航动力系航空宇航推进理论与工程专业博士

2000--2002 北航流体所博士后

2003--今天 北航宇航学院宇航推进系副教授

XIANG Hong-jun

Male

PhD，Associate Professor

Contact Information

Office: B902, New Main Building, Beijing University of Aeronautics and Astronautics

Telephone Number: 

Email Address: hjxiang@263.net

Research Interests

Combustion and flow simulation for solid rocket motor

Two-phase flow-field analysis of missile exhaust plumes

Nuclear thermal propulsion technology

Low speed preconditioning for flow computations on structured/unstructured grids

Educational

·B.S., rocket engine, Beijing University of Aeronautics and Astronautics, 1994

·M.D., space propulsion, Beijing University of Aeronautics and Astronautics, 1997

·Ph.D., space propulsion, Beijing University of Aeronautics and Astronautics, 2000

Academic Positions

·Associate Professor, Beijing University of Aeronautics and Astronautics, 2003-date

Teaching

·Computational fluid dynamics, graduate

Achievements

·Supervise more than 10 graduate students and doctoral students.

·Publish more than 10 academic papers in the domestic and foreign periodicals and conference.

研究方向

火箭发动机燃烧与流动工作过程仿真

火箭发动机两相化学反应喷流流场计算

结构网格及非结构网格下的全速度流场计算技术研究

核热能推进技术

高过载下导弹安全性研究

科研成果

长期从事火箭发动机的系统建模、流场计算、工作过程仿真等，已在国内外核心学术刊物和会议上发表学术论文多篇。承担或参与多项国家自然科学基金、863高技术项目、航天创新基金以及横向课题等。

获省部级科学技术二等奖、三等奖各一次

主讲课程

计算流体力学