研究领域

Aircraft Conceptual Design, Aircraft Aerodynamics, Computational Fluid Dynamics

论文与著作

[1]  昂海松，肖天航，郑祥明，微型飞行器设计导论，西北工业大学出版社，2012

[2]  Mingjian Wu, Tianhang Xiao, Haisong Ang, and Hongda Li.  "Optimal Flight Planning for a Z-Shaped Morphing-Wing Solar-Powered Unmanned Aerial Vehicle", Journal of Guidance, Control, and Dynamics, Vol. 41, No. 2 (2018), pp. 497-505

[3]  肖天航,罗东明,郑祥明,昂海松,吉爱红.仿生飞行器非定常气动优化设计研究进展与挑战[J].空气动力学学报,2018,36(01):80-87

[4]  Liu, Long; Li, Hongda; Ang, Haisong; Xiao, Tianhang, Numerical investigation of flexible flapping wings using computational fluid dynamics/computational structural dynamics method，PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING，2018， 232（1）：85-95

[5]  Xiao Tianhang，Qin Ning，Lu Zhaoyan，Sun Xuan，Development of a Smoothed Particle Hydrodynamics Method and its Application to Aircraft Ditching Simulations，Aerospace Science and Technology, 2017,  vol.66, pp 28-43.

[6]  Mingjian Wu, Tianhang Xiao,  Haisong Ang, Hongda Li, Optimal Flight Planning for a Z-Shaped Morphing-Wing Solar-Powered Unmanned Aerial Vehicle, Journal of Guidance Control and Dynamics, 2018, 41(2):497-505

[7]  Mingjian Wu, Tianhang Xiao, Haisong Ang, Hongda Li, Investigation of a Morphing Wing Solar-Powered Unmanned Aircraft with Enlarged Flight Latitude, Journal of Aircraft, 2017, 54(5):1-9

[8]  Zhaoyan Lu, Tianhang Xiao, Zhengzhou Li, Pitching Angle on Space Capsule Water Landing Using Smooth Particle Hydrodynamic Method, Journal of Spacecraft and Rockets , 2017, 54(3):1-12

[9]  Fanxi Lyu, Tianhang Xiao, Xiongqing Yu, A fast and automatic full-potential finite volume solver on Cartesian grids for unconventional configurations, Chinese Journal of Aeronautics, 2017, 30(3) ：951-963

[10]  Li Zhengzhou, Xiao Tianhang, Lyu Fanxi, Yu Xiongqing, et al. A Rapid Analysis Tool for Aero/Aerothermodynamics of Hypersonic Vehicles, Transactions of Nanjing University of Aeronautics & Astronautics, 2017,34 (4):1-8

[11]  卢昱锦,肖天航,李正洲. 高速平板着水数值模拟. 航空学报, 2017,38(S1)：721498

[12]  Xiao Tianhang，Qin Ning，Luo Dongming，Deng Shuanghou，Deformable Overset Grid for Multi-Body Unsteady Flow Simulation，AIAA Journal,  2016, Vol. 54, No. 8, pp. 2392-2406.

[13]  Xiao Tianhang, Li Zhengzhou, Deng Shuanghou, Ang Haisong, Zhou Xinchun, Numerical Study on the Flow Characteristics of Micro Air Vehicle Wings at Low Reynolds Numbers, International Journal of Micro Air Vehicle, 2016, vol. 8, no.1, 29-40.

[14]  黄鸣阳，肖天航，昂海松，多段柔性变体扑翼飞行器设计，航空动力学报，2016, Vol.31, No.8, pp1838-1844.

[15]  李正洲,肖天航,昂海松,陆召严. 通用导弹雷达罩曲面分片展开系统的开发[J]. 北京航空航天大学学报, 2016, 12:2715-2721

[16]  Deng Shuanghou，Xiao Tianhang，Effect of Flexion on the Propulsive Performance of a Flexible Flapping Wing，Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2016, Vol. 230(12), pp.2265–2273 (Online, DOI: 10.1177/0954410015623304)

[17]  Deng, Shuanghou，Xiao Tianhang，Bas van Oudheusden，Hester Bijl，A dynamic mesh strategy applied to the simulation of flapping wings，International Journal for Numerical Methods in Engineering, Volume 106, Issue 8, 25, May 2016, Pages 664–680   (Online, DOI:10.1002/nme.5160).

[18]  李正洲,肖天航,余雄庆. 高超声速飞行器直接阻尼动导数的快速预测方法研究[C]// 第十八届全国高超声速气动力热学术交流会会议.杭州,2016.

[19]  李正洲,肖天航,刘畅, 等.飞行器曲面外形分片展开技术与应用[C]//中国航空学会飞机总体专业分会几何设计专业第十二次学术交流会议.成都,2016

[20]  Xiao, Tianhang; Qin, Ning; Luo, Dongming; Deng, Shuanghou，Deformable Overset Grid for Unsteady Aerodynamic Simulation，54th AIAA Aerospace Sciences Meeting, 4/1/2016-9/1/2016, San Diego, 4/1/2016.

荣誉与奖励

[1] 飞机设计专业国际化综合改革与实践，南京航空航天大学教学成果二等奖，排名3，2017

[2] 直升机水上迫降着水载荷分析和试验验证技术，中航工业集团，科学技术奖三等奖，排名6，2019