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[1]肖天航,卢昱锦,邓双厚等.Hydrodynamic Characteristics of a Helicopter Ditching on Different Positions of Wavy Water[J].Journal of Aircraft,2021,58(5):1094-1105
[2]支豪林,朱震浩,卢昱锦等.Aerodynamic performance enhancement of co-flow jet airfoil with simple high-lift device[J].Chinese Journal of Aeronautics,2021,34(9):143-155
[3]肖天航,朱震浩,邓双厚.Effects of nozzle geometry and active blowing on lift enhancement for upper surface blowing configuration[J].Aerospace Science and Technology,2021,111
[4]卢昱锦,肖天航,邓双厚等.着水初始条件对水陆两栖飞机着水性能的影响[J].航空学报,2021,42(7):159-170
[5]童明波,陈吉昌,李乐等.飞行器水载荷结构完整性数值模拟现状与展望-Part I：水上迫降和水上漂浮[J].航空学报,2021,42(5):123-157
[6]付晓琴,李阳辉,卢昱锦等.二维平板水漂运动数值模拟[J].航空学报,2020,42(6):280-297
[7]Mingjian Wu,Tianhang Xiao,Haisong Ang等.Optimal Flight Planning for a Z-Shaped Morphing-Wing Solar-Powered Unmanned Aerial Vehicle[J].Journal of Guidance Control and Dynamics,2018,41(2):497-505
[8]Fanxi LYU,Tianhang XIAO,Xiongqing YU.A fast and automatic full-potential finite volume solver on Cartesian grids for unconventional configurations[J].Chinese Journal of Aeronautics,2017,30(3):951-963
[9]Zhengzhou Li,Tianhang Xiao,Fanxi Lyu等.A Rapid Analysis Tool for Aero/Aerothermodynamics of Hypersonic Vehicles[J].Transactions of Nanjing University of Aeronautics & Astronautics,2016,34(4):398-404
[10]Tianhang Xiao,Zhaoyan Lu,Shuanghou Deng.Effect of Initial Pitching Angle on Helicopter Ditching Characteristics Using Smoothed-Particle-Hydrodynamics Method[J].Journal of Aircraft,2020,58(1)
[11]肖天航,余雄庆,李正洲等.全域气动仿真工具在高超飞行器设计中的应用[J].航空计算技术,2020,50(6):18-21+26
[12]Tianhang Xiao,Zhaoyan Lu,Shuanghou Deng.Effect of Initial Pitching Angle on Helicopter Ditching Characteristics Using Smoothed-Particle-Hydrodynamics Method[J].Journal of Aircraft,2020
[13]Mingjian Wu,Zhiwei Shi,Tianhang Xiao等.Theoretical study on energy performance of a stratospheric solar aircraft with optimum Λ-shaped rotatable wing[J].Aerospace Science and Technology,2019,98
[14]李正洲,高昌,肖天航等.超/高超声速飞行器动态稳定性导数极快速预测方法[J].航空学报,2019,41(4):83-92
[15]Mingjian Wu,Zhiwei Shi,Tianhang Xiao等.Effect of solar cell efficiency and flight condition on optimal flight control and energy performance for Z-shaped wing stratospheric solar aircraft[J].Acta Astronautica,2019,164:366-375
[16]Zhenhao Zhu,Tianhang Xiao,Zhai Chen等.Numerical Study on Lift Enhancement for Upper Surface Blowing System with Powered Turbofan Engine[C].AIAA Aviation 2019 Forum,2019
[17]Yutong Jin,Haolin Zhi,Yujin Lu等.Numerical Simulation of Three Dimensional Tank Impacting on Wavy Water[C].AIAA Aviation 2019 Forum,2019
[18]Yujin Lu,Tianhang Xiao,Jichang Chen等.Numerical Simulation of Helicopter Ditching on Wavy Water[C].AIAA Aviation 2019 Forum,2019
[19]Haolin Zhi,Tianhang Xiao,Jichang Chen等.Numerical Analysis of Aerodynamics of a NACA4412 Airfoil above Wavy Water Surface[C].AIAA Aviation 2019 Forum,2019
[20]Jichang Chen,Tianhang Xiao,Lian Shen等.Numerical Wave Simulation and Investigation of Air-wave-aircraft Interactions[C].AIAA Aviation 2019 Forum,2019
[21]Mingjian Wu,Zhiwei Shi,Tianhang Xiao等.Energy optimization and investigation for Z-shaped sun-tracking morphing-wing solar-powered UAV[J].Aerospace Science and Technology,2019:1-11
[22]金禹彤,陈吉昌,卢昱锦等.楔形体入波浪水面数值模拟[J].航空学报,2019,40(10):46-59
[23]昂海松,肖天航,郑祥明.微型飞行器的低雷诺数、非定常气动设计与分析[J].无人系统技术,2018,2018(4):17-32
[24]肖天航,罗东明,郑祥明等.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(1):80-87
[25]吕凡熹,李正洲,邓经枢等.面向飞行器概念设计的全速域气动分析工具[J].空气动力学学报,2017,35(5):625-632
[26]Optimal Flight Planning for a Z-Shaped Morphing-Wing Solar-Powered Unmanned Aerial Vehicle[J].Journal of Guidance Control and Dynamics,2017,41(22):1-9
[27]王嘉,肖天航.直升机波浪迫降数值模拟[J].江苏航空,2017,2017(3):9-11
[28]卢昱锦,肖天航,李正洲.高速平板着水数值模拟[J].航空学报,2017,38(S1):6-14
[29]Mingjian Wu,Tianhang Xiao,Haisong Ang等.Investigation of a Morphing Wing Solar-Powered Unmanned Aircraft with Enlarged Flight Latitude[J].Journal of Aircraft,2017,54(5):1-9
[30]武明建,朱建辉,肖天航等.某支线客机总体方案中增升装置的设计与优化[J].南京航空航天大学学报,2017,49(3):411-419
[31]Shuanghou Deng,M. Percin,B. W. van Oudheusden等.Numerical Simulation of a Flexible X-Wing Flapping-Wing Micro Air Vehicle[J].AIAA Journal,2017,55(7):1-12
[32]Zhaoyan Lu,Tianhang Xiao,Zhengzhou Li等.Pitching Angle on Space Capsule Water Landing Using Smooth Particle Hydrodynamic Method[J].Journal of Spacecraft and Rockets,2017,54(3):1-12
[33]赵鸿渝,肖天航,李正洲.面向飞行器总体设计的快速非结构面元法及应用[J].江苏航空,2017,2017(1):40-45
[34]Tianhang Xiao,Ning Qin,Zhaoyan Lu等.Development of a smoothed particle hydrodynamics method and its application to aircraft ditching simulations[J].Aerospace Science and Technology,2017,66:28-43
[35]Fanxi Lyu,Tianhang Xiao,Xiongqing Yu.A fast and automatic full-potential finite volume solver on Cartesian grids for unconventional configurations[J].Chinese Journal of Aeronautics,2016,30(3):951-963
[36]Long Liu,Hongda Li,Haisong Ang等.Numerical investigation of flexible flapping wings using computational fluid dynamics/computational structural dynamics method[J].Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering,2016,232(1):85-95
[37]Shuanghou Deng,Tianhang Xiao.Effect of flexion on the propulsive performance of a flexible flapping wing[J].Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering,2016,230(12):2265-2273
[38]Hongda Li,Long Liu,Tianhang Xiao等.Design and simulative experiment of an innovative trailing edge morphing mechanism driven by artificial muscles embedded in skin[J].Smart Materials and Structures,2016,25(9)
[39]多段柔性变体扑翼飞行器设计[J].航空动力学报,2016,31(8):1838-1844
[40]基于自适应直角网格的二维全速势方程有限体积解法[J].计算力学学报,2016,33(3):424-430
[41]Investigation of Helicopter Ditching Angle on Fuselage Pressure Load using a SPH Method[C].46th AIAA Fluid Dynamics Conference,2016
[42]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,2016,42(12):2715-2721
[43]Deformable Overset Grid for Multibody Unsteady Flow Simulation[J].AIAA Journal,2016,53(4):2392-2406
[44]Numerical study on the flow characteristics of micro air vehicle wings at low Reynolds numbers[J].International Journal of Micro Air Vehicles,2016,8(1):29-40
[45]Deformable Overset Grid for Unsteady Aerodynamic Simulation[C].54th AIAA Aerospace Sciences Meeting,2016
[46]Numerical Investigation on the Propulsive Performance of Biplane Counter-Flapping Wings[J].International Journal of Micro Air Vehicles,2015,7(4):431-439
[47]微小型摆线桨气动特性数值研究[J].航空科学技术,2015,26(11):56-66
[48]A dynamic mesh strategy applied to the simulation of flapping wings[J].International Journal for Numerical Methods in Engineering,2015,106(8):664-680
[49]Computational fluid dynamics-based virtual flight simulation of a flying wing micro air vehicle[J].Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering,2015,230(6):1094-1102
[50]Numerical simulation of an X-wing flapping wing MAV by means of a deforming overset grid method[C].22nd AIAA Computational Fluid Dynamics Conference,2015
[51]双旋翼微型飞行器的非定常气动特性[J].航空动力学报,2015,30(1):149-154
[52]Numerical prediction of unsteady aerodynamics for a ducted fan micro air vehicle[J].Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering,2015,229(1):87-95
[53]鸭式布局战斗机非常规机动的流场机理数值分析[J].南京航空航天大学学报,2014,46(6):874-881
[54]基于CFD/CSD方法的蜻蜓柔性翼气动特性分析[J].航空动力学报,2014,29(9):2063-2069
[55]6自由度在刚体初始轨迹中的数值研究[J].机械设计与制造工程,2014,43(3):5-9
[56]柔性翼微型飞行器流固耦合数值模拟[J].南京航空航天大学学报,2013,45(5):621-627
[57]基于CFD的舰载机飞行模拟器甲板流场建模研究[J].系统仿真学报,2013,25(增刊):82-85
[58]可差动扭转扑翼飞行器的设计和风洞试验研究[J].实验流体力学,2012,27(3):35-40
[59]摆线桨气动原理及应用分析[J].西安航空技术高等专科学校学报,2013,31(1):17-20
[60]主动变形扑翼飞行器的设计和风洞测力试验研究[J].航空学报,2012,34(3):474-486
[61]微型飞行器桨翼气动干扰的数值模拟[J].航空计算技术,2012,42(2):20-23
[62]仿鸟柔性扑翼气动特性与能耗的数值研究[J].空气动力学学报,2011,29(6):709-718
[63]A preconditioned dual time-stepping procedure coupled with matrix-free LU-SGS scheme for unsteady low speed viscous flows with moving objects[J].International Journal of Computational Fluid Dynamics,2010,21((3-4)):165-173
[64]前后双扑翼水平距离及相位差对其气动性能的影响[J].计算力学学报,2010,27(4):629-633
[65]Flight mechanism and design of biomimetic micro air vehicles[J].Science in China Series E: Technological Sciences volume,2009,52(12):3722-3728
[66]蝴蝶模型的非定常气动特性研究[C].中国力学学会学术大会'2009论文摘要集,2009:467
[67]蜻蜓前后翼相位特性和气动干扰的数值研究[J].航空学报,2009,30(7):1165-1175
[68]柔性扑翼非定常流场的数值计算方法[J].航空学报,2009,30(6):990-999
[69]肖天航.低雷诺数非定常流场的数值方法及其在微型飞行器上的应用[D],2009
[70]凌维安,肖天航.基于动网格的非定常粘性空气动力学计算[J].江苏航空,2008,2008(增刊):78-81
[71]周新春,肖天航.前后双扑翼微型飞行器推力研究[J].南京航空航天大学学报,2008,40(4):460-464
[72]肖天航,昂海松,周新春.大幅度非定常运动流场分析的新方法及其在柔性扑翼上的应用[C].探索 创新 交流——第三届中国航空学会青年科技论坛文集（第三集）,2008:202-209
[73]Tianhang Xiao,Haisong Ang.COMBINATION OF MESH DEFORMATION AND OVERSET GRID FOR SIMULATING UNSTEADY FLOW OF INSECT FLIGHT[J].Modern Physics Letters B,2008,23(3):525-528
[74]朱保利,肖天航,昂海松等.微飞行器前后同频双扑动翼的推进效果[J].清华大学学报(自然科学版),2008,48(2):298-301
[75]肖天航,昂海松,仝超.大幅运动复杂构形扑翼动态网格生成的一种新方法[J].航空学报,2008,29(1):41-48
[76]肖天航,昂海松,余少志等.预处理法求解定常/非定常混合网格的全速流场[J].空气动力学报,2007,25(4):425-430+442
[77]周新春,昂海松,肖天航等.微飞行器前后同频双扑动翼的推进效果[J].清华大学学报(自然科学版)网络.预览,2007,48(2):298-301
[78]昂海松,肖天航.运动边界非定常全速流场的数值模拟[C].非定常空气动力学研讨会论文选集,2007,26(增刊):73-79
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