李新田
个人信息
Personal information
教师英文名称：Lixintian
职称：副研究员（自然科学）
硕士生导师
学科：仪器科学与技术
所在单位：智能科学与技术学院
电子邮箱：
手机版二维码
Mobile QR code
- [11] Li Xintian*, Tian Hui, Zeng Peng, Yu Nanjia, Cai Guobiao. Three-dimensional numerical simulation of the flow field in hybrid rocket motor with wagon-wheel fuel grain[A]. 63rd International Astronautical Congress[C], IAC-12, C4,2,19,x13996. （EI Number: 20133716731415）.
- [12] Li Xintian*, Tian Hui, Yu Nanjia, Cai Guobiao. Three-dimensional numerical simulation of two-phase flow in hybrid rocket motor [A]. 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit [C], San Jose, California, Ju+B35l. 14-17, 2013, AIAA 2013-3893. （EI Number: 20133816751285）.
- [13] Tian Hui, Li Xintian, Yu Nanjia, Cai Guobiao*. Numerical and experimental investigation on the effects of aft mixing chamber diaphragm in hybrid rocket motor [J]. Sci China Tech Sci. 2013, 56(11): 2721-2731. Doi: 10.1007/s11431-013-5325-z. （SCI: 000326459800015 ）.
- [14] Tian Hui, Li Xintian*, Cai Guobiao. Ignition theory investigation and experimental research on hybrid rocket motor [J]. Aerospace Science and Technology, 2015, 42: 334-341. Doi: 10.1016/j.ast.2015.01.015.（SCI: 000352332600035）.
- [15] Tian Hui, Li Xintian*, Zeng Peng, Yu Nanjia, Cai Guobiao. Numerical and experimental studies of the hybrid rocket motor with multi-port fuel grain [J]. Acta Astronautica. 2014, 96: 261-268. Doi: 10.1016/j.actaastro.2013.12.001. （SCI: 000331666400026 ）.
- [16] Li Xintian, Tian Hui*, Yu Nanjia, Cai Guobiao. Experimental investigation of fuel regression rate in HTPB based lab-scale hybrid rocket motor [J]. Acta Astronautica. 2014, 105: 95-100. Doi: 10.1016/j.actaastro.2014.08.028. （SCI: 000347021400012 ）.
- [17] Li Xintian, Tian Hui*, Yu Nanjia, Cai Guobiao. Experimental investigation of combustion in axial-injection end-burning hybrid rocket motor[J]. Journal of Propulsion and Power. 2015, 31(3): 930-936. （SCI: 000360839900017 ）.
- [18] Li Xintian, Tian Hui, Cai Guobiao*. Numerical analysis of fuel regression rate distribution characteristics of hybrid rocket motor with different fuel types [J]. Sci China Tech Sci. 2013, 56(7): 1807-1817. Doi: 10.1007/s11431-013-5251-0. （SCI: 000320891800027 ）.