近期论文
查看导师最新文章
（温馨提示：请注意重名现象，建议点开原文通过作者单位确认）
多层次转捩（DNS 1-4、RANS-LES混合5-8、转捩模式9-15、稳定性分析16-17）
Bai T, Duan ZW & Xiao ZX*, Depth effects on the cavity induced transition at hypersonic speed by DNS. International Journal of Heat and Fluid Flow 97 (109028) : 1-16, 2022.
Duan ZW & Xiao ZX *, Effects of external disturbances on the diamond-induced transition by DNS. AIAA Journal, 60（2）：731-746，2022.
Duan ZW and Xiao ZX*，Hypersonic transition induced by three isolated roughness elements on a flat plate. Computers and Fluids, 157, 1-13, 2017.
Duan ZW, Xiao ZX* and Fu S. Direct numerical simulation of hypersonic transition induced by an isolated cylindrical roughness element. Science China Physics, Mechanics & Astronomy, 57(12), 2330-2345, 2014.
Wang GX, Xiao ZX* & Chen LZ. Simultaneous simulation of transition and massive separation by RANS-LES-Tr model. Aerospace Science and Technology, 105, 106026, 2020.
Cui WY, Xiao ZX* & Yuan XJ. Simulations of transition and separation past a wind-turbine airfoil near stall. Energy, 205, 118003, 2020.
Xiao ZX *, Wang GX, Yang MC, Chen LZ. Numerical investigations of hypersonic transition and massive separation past Orion capsule by DDES-Tr. International Journal of Heat and Mass Transfer, 137, 90-107, 2019.
Xiao LH, Xiao ZX, Duan ZW and Fu S*. Improved-delayed-detached-eddy simulation of cavity-induced transition in hypersonic boundary layer. International Journal of Heat and Fluid Flow, 51, 138-150, 2015.
Yang MC & Xiao ZX*. Improving the k-ω-γ-Ar transition model using the field inversion and machine learning framework. Physics of Fluids, 32, 064101, 2020.
Yang MC & Xiao ZX*. Parameter uncertainty quantification for a four-equation transition model using a data assimilation approach. Renewable Energy. 158, 215-226, 2020.
Yang MC & Xiao ZX*. POD-based surrogate modeling of transitional flows using an adaptive sampling in Gaussian process. International Journal of Heat and Fluid Flow. 84, 108596, 2020.
Yang MC and Xiao ZX*, Distributed roughness induced transition on wind-turbine airfoils simulated by four-equation k-omega-gamma-Ar transition model. Renewable Energy, 135, 166-177, 2019.
Liu J, Xiao ZX* & Fu S. Investigations of unsteady transition flows over a pitching airfoil using a k-w-g transition model. AIAA Journal, 56（9），3776-3781，2018.
Wang GX, Yang MC, Xiao ZX* & Fu S. Improved k-w-g transition model by introducing the local effects of nose bluntness for hypersonic heat transfer. International Journal of Heat and Mass Transfer, 119, 185-198, 2018.
Zhao M, Xiao ZX and Fu S*, Predictions of transition on a hovering tilt-rotor blade. Journal of Aircraft, 51(6), 1094-1103, 2014.
Xu GL, Xiao ZX and Fu S*. Secondary instability control of compressible flow by suction for a swept wing. Science China Physics, Mechanics & Astronomy, 54(11), 2040-2052, 2011.
Xu GL, Xiao ZX and Fu S*. Analysis of the secondary instability of the incompressible flows over a swept wing. Science China Physics, Mechanics & Astronomy, 54(4), 724-736, 2011.
宽速域RANS-LES混合模型及其应用
Liu J, Chen JQ, Ren HX, Zhang Y, He XY, Xiao ZX*, Correlations of unsteady vortex burst point and dynamic stability over a pitching double-delta wing. Aerospace Science and Technology. 107, 106256, 2020.
Liu J, Xiao ZX *, Low-Frequency Oscillation over NACA0015 Airfoil Near Stall at High Reynolds Number. AIAA Journal, 58(1), 53-60, 2020.
Zhu WQ, Xiao ZX* & Fu S. Numerical modeling screen for flow and noise control around tandem cylinders. AIAA Journal, 58 (6), 2504-2516, 2020.
Zhu WQ, Xiao ZX * & Fu S. Studies of flight-velocity effects on near-field and intermittent properties of a subsonic jet. Computers & Fluids, 196, 104351, 2020.
Wang B, Liu J, Xiao ZX* and Yang YJ. Numerical studies of undulation control on dynamic stall for reverse flows. Acta Mechanics Sinica. 36, 290–305, 2020.
Wang B, Liu J, Li QB, Yang YJ and Xiao ZX*, Numerical studies of reverse flows controlled by undulating leading edge. Science China Physics, Mechanics & Astronomy, 62(7)，94712, 2019.
Liu J, Zhu WQ, Xiao ZX*, Sun HS, Huang Y & Liu ZT. DDES with adaptive coefficient for stalled flows past a wind-turbine airfoil. Energy, 161,846-858, 2018.
Liu J, Luo KY, Sun HS, HY, Liu ZT & Xiao ZX*. Dynamic response of vortex breakdown flows to a pitching double-delta wing. Aerospace Science and Technology, 72, 564-577, 2018.
Cui WY, Liu J, Sun YH, Li QB, and Xiao ZX*. Airbrake controls of pitching moment and pressure fluctuation for an oblique tail fighter model. Aerospace Science and Technology, 81,294-305，2018.
Tan S, Li QB*, Xiao ZX and Fu S. Gas kinetic scheme for turbulence simulation, Aerospace Science and Technology, 78, 214-227, 2018.
Luo KY, Zhu WQ, Xiao ZX*, Weng Z, Deng LD, Liu J & Yang DG, Investigations on spectral characteristics of passive controls in a supersonic cavity flow. AIAA Journal, 56（7），2669-2686，2018.
Luo KY, Weng Z, Xiao ZX* & Fu S. Improved delayed detached-eddy simulations of sawtooth spoiler control before supersonic cavity. International Journal of Heat and Fluid Flow, 63, 172-189, 2017.
Xiao ZX* and Luo KY. Improved delayed detached-eddy simulations of massive separation around triple cylinders. Acta Mechanica Sinica. 31(6), 799–816, 2015.
Liu J, Sun HS, Liu ZT, Xiao ZX*, Numerical investigation on unsteady vortex breakdown past the 80°/65° double-delta wing. Chinese Journal of Aeronautics, 27(3), 521-530, 2014.
Xiao ZX, Liu J, Luo KY, Huang JB and Fu S*. Numerical investigation of massively separated flows past rudimentary landing gear using advanced DES approaches. AIAA Journal, 51(1), 107-125, 2013.
Xiao ZX, Liu J, Huang JB and Fu S*. Numerical dissipation effects on the massive separation around tandem cylinders. AIAA Journal, 50(5), 1119-1136, 2012
Huang JB, Xiao ZX, Liu J and Fu S*. Simulation of shock wave buffet and its suppression on an OAT15A supercritical airfoil by IDDES. Science China Physics, Mechanics & Astronomy, 55(2), 260-271, 2012.
Xiao ZX*, Liu J and Fu S. Predictions of massive separation around landing-gear-like geometries. Journal of Hydrodynamics, 22(5), 883-888, 2010.
Xiao ZX* and Fu S. Studies of the unsteady supersonic base flows around three afterbodies. ACTA Mechanics Sinica，25, 471-479, 2009.
Xiao ZX*, Zhang YF, Huang JB, Chen HX and Fu S. Prediction of separation flows around a 6:1 prolate spheroid using RANS/LES hybrid approaches. ACTA Mechanics Sinica, 23(4), 369–382, 2007.
Fu S*, Xiao ZX, Chen HX, Zhang YF, and Huang JB. Simulation of wing-body junction flows with hybrid RANS/LES methods. International Journal of Heat and Fluid Flow, 28, 1379-1390, 2007.
Xiao ZX*, Chen HX, Zhang YF, Huang JB and Fu S. Study of delayed-detached eddy simulation with weakly nonlinear turbulence model. Journal of Aircraft, 43(5), 1377-1385, 2006.
其他
Liu J, Chen JQ, Zhang ZP, Yang YF and Xiao ZX*. Assessment of a new hybrid-SSOR implicit temporal scheme for turbulent flows across a wide range of Mach numbers. Acta Mechanica Sinica, 39 (322398) : 1-10, 2023.
Xie ZX, Xiao ZX, Wang G and Yang YG*. Direct numerical simulation of the effects of Reynolds number in Mach 2.9 flows over an expansion–compression corner. Physics of Fluids, 34 (125129) : 1-20, 2022.
Huang HX, Tan HJ*, Lin ZK, Li ZJ, Sun S, Chen H, Xiao ZX, Flowfield of a helicopter submerged inlet with power output shaft. Acta Mechanica Sinica, 37(1), 156–168, 2021.
Xie Q, Xiao ZX, Ren ZY*, A spectral radius scaling semi-implicit iterative time stepping method for reactive flow simulations with detailed chemistry, Journal of Computational Physics, 368, 47-68，2018.
Liu J, Sun HS, Huang Y, Jiang Y, Xiao ZX*，Numerical investigation of an advanced aircraft model during pitching motion at high incidence. Science China –Technological Sciences, 59(2), 276-288, 2016.
Huang JB，Xiao ZX and Fu S*, Study of control effects of vortex generators on a supercritical wing. Science China –Technical Sciences, 53, 2038-2048, 2010.
Xiao ZX*, Chen HX, Fu S and Li FW. Computations with k-g model for complex configurations at high-incidence. Journal of Aircraft, 42(2), 462-468, 2005.
邀请报告
肖志祥，高超声速边界层转捩模拟及解析，中国运载火箭技术研究院科技委气水动专业组气动专业“开讲啦”系列讲座，2022年12月26日，线上。
肖志祥，宽速域RANS-LES混合方法及其应用，深海技术科学太湖实验室蛟龙讲堂，2022年11月26日，线上。
肖志祥，吸气式飞行器进气道起动边界及抗反压能力研究， M4级组合动力进排气设计与试验技术研讨咨询会，2021年12月1日，四川成都.
肖志祥，宽速域RANS-LES混合方法中的自适应耗散格式，HOMA-CFD-2021，2021年7月23-25日，上海大学，上海.
肖志祥*，宽速域RANS-LES混合方法及其应用，中国科学院力学研究所，2021年6月2日，北京.
肖志祥*，高超声速边界层转捩及非定常湍流数值仿真，国防科学技术大学，2021年4月9日，湖南长沙.
肖志祥*，转捩与非定常分离流动一体数值预测，空气动力学四季学术论坛，2021年3月9日,中国航天空气动力研究院，北京.
肖志祥*，基于数据驱动的四方程转捩模式研究，数据智能赋能流体力学学术研讨会，2020年11月，西北工业大学，陕西西安.
肖志祥*，RANS-LES混合方法框架体系，2020年7月23日，中国空气动力研究与发展中心，四川绵阳.
肖志祥*，发动机喷流与机翼安装效应对气动噪声的影响研究，2019年11月28日，2019超级云计算应用年会暨AMD HPC应用研讨会，北京.
肖志祥*，RANS-LES混合方法框架体系，第15届全国高性能计算学术年会-航空航天领域高性能计算应用论坛，2019年8月24日，内蒙古呼和浩特.
Xiao ZX*, Simultaneous studies of flows with transition and massive separation, Int. Symposium on High-Fidelity Computational Methods & Applications, 14-16, Dec, 2019, Shanghai.
肖志祥*，高超声速转捩与湍流过程中流动结构的精细预测，第十三届中国系统建模与仿真技术高层论坛，2018年10月30-31日，北京.
肖志祥*，高超声速边界层转捩模拟及解析，中国科学技术大学，2018年5月27日，安徽合肥.
Xiao ZX*，Unsteady flows and airframe noise past landing gear-like geometries, 1st Advanced AeroAcoustics Workshop, Nov.29-30, 2017, BUAA, Beijing.
肖志祥*，转捩与非定常湍流预测进展，西北工业大学力学论坛暨第一届“力学日”， 2017年11月2~4日，西安.
肖志祥*，刘健，罗堃宇，RANS-LES混合方法对非定常载荷的精细模拟，中国航空学会空气动力学分会飞行载荷专业委员会第一届学术交流会，2016年12月8-9日，广东珠海.
肖志祥*，进气道不起动影响因素研究，第五届冲压发动机技术交流会， 2015年9月23-25日，福建厦门.
Xiao ZX & Fu S*. Simulations of Complex Turbulent Flows with RANS-LES Hybrid Approaches. 3rd symposium on Fluid-Structure-Sound interactions and Control (FSSIC3), July 5 – 9, 2015, Perth, Australia.
肖志祥*，IDDES方法在LAST实验室内的应用及展望，中国力学大会-2013——“RANS/LES混合方法研究进展”专题研讨会，2013年8月，陕西西安.
肖志祥*，起落架类非定常大范围分离流动预测，中国空气动力学学会CFD专业委员会, 2011年9月，福建武夷山.
肖志祥*，RANS/LES混合方法及其应用，中国力学大会-暨钱学森诞辰100周年纪念大会——流体力学分会场，2011年8月，黑龙江哈尔滨.
Fu S *, Xiao ZX, Huang JB and Zhang YF, Investigation of Practical Flow Control Methodologies with RANS/LES Hybrid Methods, 3rd Symposium on RANS/LES Hybrid Methods, June 2009, Gdansk, Poland.
京公网安备 11010802027423号