1.粗糙元诱导的高超声速边界层转捩

段志伟,肖志祥

航空学报[1000-6893], Published 2016, Issue 08, Pages 2454-2463

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2.Numerical investigation of an advanced aircraft model during pitching motion at high incidence

Liu, J, Sun, HS, Huang, Y, Jiang, Y, Xiao, ZX

SCIENCE CHINA-TECHNOLOGICAL SCIENCES[1674-7321], Published 2016, Volume 59, Issue 2, Pages 276-288

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3.Simulations of Complex Turbulent Flows with RANS-LES Hybrid Approaches

Xiao, ZX, Fu, S, Zhou, Y, Lucey, AD, Liu, Y, Huang, L

FLUID-STRUCTURE-SOUND INTERACTIONS AND CONTROL[2195-4356], Published 2016, Pages 271-281

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4.Improved-Delayed-Detached-Eddy Simulation of cavity-induced transition in hypersonic boundary layer

Xiao, Lianghua, Xiao, Zhixiang, Duan, Zhiwei, Fu, Song

International Journal of Heat and Fluid Flow[0142-727X], Published 2015, Volume 51, Pages 138-150

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5.Improved delayed detached-eddy simulation of transonic and supersonic cavity flows

Luo, Kunyu, Xiao, Zhixiang

Notes on Numerical Fluid Mechanics and Multidisciplinary Design[1612-2909], Published 2015, Volume 130, Pages 163-174

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6.Improved delayed detached-eddy simulation of massive separation around triple cylinders

Xiao, ZX, Luo, KY

ACTA MECHANICA SINICA[0567-7718], Published 2015, Volume 31, Issue 6, Pages 799-816

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7.Direct numerical simulation of hypersonic transition induced by an isolated cylindrical roughness element

Duan, ZW, Xiao, ZX, Fu, S

SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY[1674-7348], Published 2014, Volume 57, Issue 12, Pages 2330-2345

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8.Predictions of Transition on a Hovering Tilt-Rotor Blade

Zhao, M, Xiao, ZX, Fu, S

JOURNAL OF AIRCRAFT[0021-8669], Published 2014, Volume 51, Issue 6, Pages 1904-1913

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9.Numerical investigation of unsteady vortex breakdown past 80 degrees/65 degrees double-delta wing

Liu, J, Sun, HS, Liu, ZT, Xiao, ZX

CHINESE JOURNAL OF AERONAUTICS[1000-9361], Published 2014, Volume 27, Issue 3, Pages 521-530

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10.Predictions of transition on a hovering tilt-rotor blade

Zhao, Ming, Xiao, Zhixiang, Fu, Song

52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014, Published 2014,

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11.Direct numerical simulation of hypersonic transition induced by ramp roughness elements

Duan, Zhiwei, Xiao, Zhixiang, Fu, Song

52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014, Published 2014,

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12.Direct numerical simulation of geometrical parameter effects on the hypersonic ramp-induced transition

Duan, Zhiwei, Xiao, Zhixiang

AIAA AVIATION 2014 -7th AIAA Theoretical Fluid Mechanics Conference, Published 2014,

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13.翼面吸气混合层流控制的数值研究

张驰宇,肖志祥,邓一菊

中国科学:物理学 力学 天文学[1674-7275], Published 2014, Issue 09, Pages 944-954

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14.Investigation of Flows Around a Rudimentary Landing Gear with Advanced Detached-Eddy-Simulation Approaches

Xiao, ZX, Liu, J, Luo, KY, Huang, JB, Fu, S

AIAA JOURNAL[0001-1452], Published 2013, Volume 51, Issue 1, Pages 107-125

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15.A modular RANS approach for modeling hypersonic flow transition on an air-breathing configuration

Xiao, Lianghua, Wang, Liang, Xiao, Zhixiang, Fu, Song

51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013, Published 2013,

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16.Numerical simulations of the near-field flows past cylinders in tandem arrangements

Xiao, Zhixiang, Luo, Kunyu

51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013, Published 2013,

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17.Direct numerical simulation of hypersonic transition induced by a cylindrical roughness element

Duan, Zhiwei, Xiao, Zhixiang, Fu, Song

43rd Fluid Dynamics Conference, Published 2013,

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18.Studies of roughness-induced transition using three-quation κ-ω-γ transition/turbulence model

Xiao, Zhixiang, Zhang, Minghua, Xiao, Lianghua, Fu, Song

43rd Fluid Dynamics Conference, Published 2013,

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19.Numerical simulations of tandem cylinders with subcritical spacing

Xiao, Zhixiang, Luo, Kunyu

19th AIAA/CEAS Aeroacoustics Conference, Published 2013, Pages 199

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20.Numerical Dissipation Effects on Massive Separation Around Tandem Cylinders

Xiao, ZX, Liu, J, Huang, JB, Fu, S

AIAA JOURNAL[0001-1452], Published 2012, Volume 50, Issue 5, Pages 1119-1136

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21.Simulation of shock wave buffet and its suppression on an OAT15A supercritical airfoil by IDDES

Huang, Jingbo, Xiao, Zhixiang, Liu, Jianguo, Fu, Song

Science China: Physics, Mechanics and Astronomy[1674-7348], Published 2012, Volume 55, Issue 2, Pages 260-271

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22.Comparisons of three improved des methods on unsteady flows past tandem cylinders

Xiao, Zhixiang, Liu, Jianguo, Huang, Jingbo, Fu, Song

Notes on Numerical Fluid Mechanics and Multidisciplinary Design[1612-2909], Published 2012, Volume 117, Pages 231-243

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23.Numerical investigation of shock buffet on an oat15a airfoil and control effects of vortex generators

Huang, Jingbo, Xiao, Zhixiang, Liu, Jianguo, Fu, Song

50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Published 2012,

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24.Numerical investigations of massively separated flows past Rudimentary Landing Gear using SST-DDES

Xiao, Zhixiang, Liu, Jianguo, Luo, Kunyu, Huang, Jingbo, Fu, Song

50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Published 2012,

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25.Numerical investigation of massively separated flows past RLG using advanced DES approaches

Xiao, Zhixiang, Liu, Jian, Luo, Kunyu, Huang, Jingbo, Fu, Song

18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), Published 2012,

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26.Simulation of transition triggered by isolated roughness in hypersonic boundary layer

Duan, Zhiwei, Xiao, Zhixiang, Fu, Song

42nd AIAA Fluid Dynamics Conference and Exhibit 2012, Published 2012,

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27.Investigate of passive flow control methodologies using SST-IDDES

Xiao, Zhixiang, Duan, Zhiwei, Huang, Jingbo, Fu, Song

28th Congress of the International Council of the Aeronautical Sciences 2012, ICAS 2012, Published 2012, Volume 2, Pages 1669-1676

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28.高升力多段机翼的转捩预测研究

肖良华,肖志祥,王丽莎,符松,曾宏刚,黎军

中国科学:物理学 力学 天文学[1674-7275], Published 2012, Issue 03, Pages 271-281

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29.第四届国际雷诺平均–大涡模拟混合方法学术会议纪要

罗堃宇,肖志祥,符松

力学进展[1000-0992], Published 2012, Issue 02, Pages 222-225

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30.Secondary instability control of compressible flow by suction for a swept wing

Xu, GL, Xiao, ZX, Fu, S

SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY[1674-7348], Published 2011, Volume 54, Issue 11, Pages 2040-2052

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31.Analysis of the secondary instability of the incompressible flows over a swept wing

Xu, GL, Xiao, ZX, Fu, S

SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY[1674-7348], Published 2011, Volume 54, Issue 4, Pages 724-736

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32.Study into effects of vortex generators on a supercritical wing

Huang, Jingbo, Fu, Song, Xiao, Zhixiang

Computational Fluid Dynamics 2010 - Proceedings of the 6th International Conference on Computational Fluid Dynamics, ICCFD 2010, Published 2011, Pages 309-314

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33.Unsteady flow around two tandem cylinders using advanced turbulence modeling method

Liu, Jian, Xiao, Zhixiang, Fu, Song

Computational Fluid Dynamics 2010 - Proceedings of the 6th International Conference on Computational Fluid Dynamics, ICCFD 2010, Published 2011, Pages 879-881

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34.Study into Effects of Vortex Generators on a Supercritical Wing

Huang, JB, Xiao, ZX, Fu, S, Kuzmin, A

COMPUTATIONAL FLUID DYNAMICS 2010, Published 2011, Pages 309-314

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35.Unsteady Flow Around Two Tandem Cylinders Using Advanced Turbulence Modeling Method

Liu, J, Xiao, ZX, Fu, S, Kuzmin, A

COMPUTATIONAL FLUID DYNAMICS 2010, Published 2011, Pages 879-881

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36.Calculations of massive separation around landing-gear-like geometries

Xiao, ZX, Liu, J, Fu, S

JOURNAL OF HYDRODYNAMICS[1001-6058], Published 2010, Volume 22, Issue 5, Pages 883-888

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37.Study of control effects of vortex generators on a supercritical wing

Huang, JB, Xiao, ZX, Fu, S, Zhang, MA

SCIENCE CHINA-TECHNOLOGICAL SCIENCES[1674-7321], Published 2010, Volume 53, Issue 8, Pages 2038-2048

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38.超临界机翼表面涡流发生器影响研究

黄静波,肖志祥,符松,张淼

中国科学:技术科学[1674-7259], Published 2010, Issue 08, Pages 867-878

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39.Investigation of Practical Flow Control Methodologies with RANS/LES Hybrid Methods

Fu, S, Xiao, ZX, Huang, JB, Zhang, YF, Peng, SH, Doerffer, P, Haase, W

PROGRESS IN HYBRID RANS-LES MODELLING[1612-2909], Published 2010, Volume 111, Pages 41-58

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40.Studies of the unsteady supersonic base flows around three afterbodies

Xiao, Zhixiang, Fu, Song

Acta Mechanica Sinica/Lixue Xuebao[0567-7718], Published 2009, Volume 25, Issue 4, Pages 471-479

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41.Drag reduction through controlling separation on the missile afterbodies

Xiao, Zhixiang, Zhou, Keke, Fu, Song

Yuhang Xuebao/Journal of Astronautics[1000-1328], Published 2009, Volume 30, Issue 5, Pages 1770-1807

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42.用RANS/LES混合方法研究超声速底部流动

肖志祥,符松

计算物理[1001-246X], Published 2009, Issue 02, Pages 221-230

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43.导弹表面流动分离与后体减阻设计

肖志祥,周克克,符松

宇航学报[1000-1328], Published 2009, Issue 05, Pages 1770-1776+1807

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44.Simulation of wing-body junction flows with hybrid RANS/LES methods

Fu, S, Xiao, ZX, Chen, HX, Zhang, YF, Huang, JB

INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW[0142-727X], Published 2007, Volume 28, Issue 6, Pages 1379-1390

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45.Prediction of separation flows around a 6 : 1 prolate spheroid using RANS/LES hybrid approaches

Xiao, ZX, Zhang, YF, Huang, JB, Chen, HX, Fu, S

ACTA MECHANICA SINICA[0567-7718], Published 2007, Volume 23, Issue 4, Pages 369-382

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46.Analysis of vortex shedding modes of an in-line oscillating circular cylinder in a uniform flow

Zhang, Yufei, Xiao, Zhixiang, Fu, Song

Lixue Xuebao/Chinese Journal of Theoretical and Applied Mechanics[0459-1879], Published 2007, Volume 39, Issue 3, Pages 408-416

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47.流向强迫振荡圆柱绕流的涡脱落模态分析

张宇飞,肖志祥,符松

力学学报[0459-1879], Published 2007, Issue 03, Pages 408-416

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48.Primary study of transitions in turbulence models

Xiao, Zhixiang, Chen, Haixin, Li, Qibing, Fu, Song

Jisuan Wuli/Chinese Journal of Computational Physics[1001-246X], Published 2006, Volume 23, Issue 1, Pages 61-65

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49.Numerical simulation for transonic flows at high incidence around a complete fighter with two-equation k-g model

Xiao, Zhixiang, Chen, Haixin, Fu, Song, Li, Fengwei

Jisuan Lixue Xuebao/Chinese Journal of Computational Mechanics[1007-4708], Published 2006, Volume 23, Issue 1, Pages 13-18

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50.Simulation of separation flows with RANS/LES hybrid methods

Xiao, Zhixiang, Chen, Haixin, Li, Qibing, Fu, Song

Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica[0258-1825], Published 2006, Volume 24, Issue 2, Pages 218-222

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51.Study of delayed-detached eddy simulation with weakly nonlinear turbulence model

Xiao, Zhixiang, Chen, Haixin, Zhang, Yufei, Huang, Jingbo, Fu, Song

Journal of Aircraft[0021-8669], Published 2006, Volume 43, Issue 5, Pages 1377-1385

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52.Prediction for separation flows around a 6:1 prolate spheroid using hybrid RANS/LES methods

Xiao, Zhixiang, Chen, Haixin, Zhang, Yufei, Huang, Jingbo, Fu, Song

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting, Published 2006, Volume 14, Pages 10756-10764

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53.湍流模式对转捩的初步研究

肖志祥,陈海昕,李启兵,符松

计算物理[1001-246X], Published 2006, Issue 01, Pages 61-65

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54.两方程k-g模式在全机大迎角流场中的应用研究

肖志祥,陈海昕,符松,李凤蔚

计算力学学报[1007-4708], Published 2006, Issue 01, Pages 13-18

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55.采用RANS/LES混合方法研究分离流动

肖志祥,陈海昕,李启兵,符松

空气动力学学报[0258-1825], Published 2006, Issue 02, Pages 218-222

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56.Computations with k-g model for complex configurations at high-incidence

Xiao, Zhixiang, Chen, Haixin, Fu, Song, Li, Fengwei

Journal of Aircraft[0021-8669], Published 2005, Volume 42, Issue 2, Pages 462-468

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57.Asymmetrical vortex breakdown of delta wings at high incidence

Xiao, Zhixiang, Fu, Song, Chen, Haixin, Li, Fengwei

Jisuan Wuli/Chinese Journal of Computational Physics[1001-246X], Published 2005, Volume 22, Issue 3, Pages 221-226

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58.Numerical study of separation flows with LES/RANS hybrid appoaches

Xiao, Zhixiang, Chen, Haixin, Fu, Song

4th International Symposium on Turbulence and Shear Flow Phenomena, Published 2005, Volume 2, Pages 577-582

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59.三角翼大迎角非对称旋涡破裂数值模拟

肖志祥,陈海昕,符松,李凤蔚

计算物理[1001-246X], Published 2005, Issue 03, Pages 221-226

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60.Simulation of shock/boundary interaction flows with several temporal and spatial schemes

Xiao, Zhixiang, Chen, Haixin, Fu, Song, Li, Fengwei

Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University[1000-2758], Published 2004, Volume 22, Issue 6, Pages 800-805

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61.The numerical calculation about flow-fields at high alpha of complete aircraft geometry with two-equation k-g model

Xiao, Zhixiang, Chen, Haixin, Fu, Song, Li, Fengwei

AIAA Paper, Published 2004, Pages 11445-11452

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62.激波/边界层干扰流动数值模拟格式的应用研究

肖志祥,陈海昕,李凤蔚,符松

西北工业大学学报[1000-2758], Published 2004, Issue 06, Pages 800-805

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