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2017.6-½ñ£¬Î÷±±¹¤Òµ´óѧ£¬½ÌÊÚ2015.1-½ñ £¬Î÷±±¹¤Òµ´óѧ£¬º½¿ÕѧԺÁ÷ÌåÁ¦Ñ§Ïµ¸±Ö÷ÈΣ¨¸ºÔðÑо¿Éú½Ìѧ¡¢ÕÐÉúµÈ£©?????????????????£¨2016.1£¬±»ÆƸñƸÈÎΪ½ÌÊÚ¸Ú룩2013.8-2014.8£¬ÃÀ¹úÂõ°¢ÃÜ´óѧ£¬¹¤³ÌѧԺ»úеÓ뺽¿Õº½Ì칤³Ìϵ£¬·ÃÎÊѧÕß2011.7-2017.6£¬Î÷±±¹¤Òµ´óѧ£¬º½¿ÕѧԺÁ÷ÌåÁ¦Ñ§Ïµ£¬¸±½ÌÊÚ£¬Ë¶Ê¿Éúµ¼Ê¦2009.7-2011.7£¬Î÷±±¹¤Òµ´óѧ£¬º½¿ÕÓ¿ÆѧÓë¼¼Êõ²©Ê¿ºóÁ÷¶¯Õ¾£¬²©Ê¿ºó£¬¸±½ÌÊÚ£¨2011.4£© Ö÷³ÖÏîÄ¿£º1¡¢¹ú¼Ò×ÔÈ»¿Æѧ»ù½ðÃæÉÏÏîÄ¿£¬2015.01-2018.122¡¢¹ú¼Ò×ÔÈ»¿Æѧ»ù½ðÇàÄêÏîÄ¿£¬2013.01-2015.123¡¢Ãñ»úרÏîÔ¤ÑÐÏîÄ¿×ÓרÌ⣬2016.01-2018.124¡¢ÉÂÎ÷Ê¡×ÔÈ»¿Æѧ»ù½ð£¬2016.01-2017.125¡¢º½¿Õ¿Æѧ»ù½ð£¬2016.10-2018.096¡¢×Ü×°±¸²¿Ô¤Ñлù½ð2Ï2016.10-2018.09£¬2010.04-2012.037¡¢ÉîÛÚÊлù´¡Ñо¿ÏîÄ¿£¬2016.06-2018.058¡¢Î÷±±¹¤Òµ´óѧ»ù´¡Ñо¿»ù½ð2Ï2015.01-2015.12£¬2012.01-2013.129¡¢Öйú²©Ê¿ºó¿Æѧ»ù½ð£¬2010.09-2012.08 ·¢±íÂÛÎĹ²30Óàƪ£¬ÆäÖеÚÒ»×÷ÕßSCIÆÚ¿¯ÂÛÎÄ 13 ƪ£¬EIË÷Òý½ü30ƪ¡£Ó¢ÎÄÂÛÎÄ·¢±í£º[1] XuHe-Yong*,Dong Qing-Li, Qiao Chen-Liang, Ye Zheng-Yin. Flow Control over theBlunt Trailing Edge Wind Turbine Airfoil Using Circulation Control. Energies,2018,11(3): 619.?£¨SCIÔ´¿¯£©?[2]Xu He-Yong*, Qiao Chen-Liang, Yang Hui-Qiang, Ye Zheng-Yin. Active Circulation Control on the Blunt Trailing Edge Wind Turbine Airfoil. AIAA Journal, 2018,56(2): 554-570. £¨SCI£º**010£¬EI£º**693£©? [3] Xu He-Yong*, Yang Hui-Qiang, Ye Zheng-Yin, Zhang Dong. Numerical Study of the Discrete Staggered Staged Sonic Jet Interaction in a Supersonic Crossflow. AIAA Paper 2017-2147. 21st AIAA International Space Planes and Hypersonics Technologies Conference, 6-9 March 2017, Xiamen, China. (EI: **668)?[4] Xu He-Yong*, Qiao Chen-Liang,Yang Hui-Qiang, Ye Zheng-Yin. Delayed Detached Eddy Simulation of the WindTurbine Airfoil S809 for Angles of Attack up to 90 Degrees. Energy,2017, 118: 1090-1109.? £¨SCI£º**093? , EI: **354£©?(ÎåÄêƽ¾ùIF=5.18£¬¹¤³Ì¼¼Êõ1ÇøtopÆÚ¿¯)?[5] Xu He-Yong*, Xing Shi-Long,Ye Zheng-Yin, Ma Ming-Sheng. A simple and conservative unstructuredsliding-mesh approach for rotor-fuselage aerodynamic interaction simulation. Proceedingsof the institution of Mechanical Engineers Part G: Journal of AerospaceEngineering, 2017, 231(1): 163-179. £¨SCI: **012?, EI: **068£©?[6] Xu He-Yong*, Qiao Chen-Liang,Ye Zheng-Yin. Dynamic Stall Control on the Wind Turbine Airfoil via a Co-FlowJet. Energies,2016, 9(6), 429:1-25. (SCI£º**042)?[7] XuHe-yong*, Xing Shi-long, Ye Zheng-yin. Numerical Study of anAirfoil/Rotating-Slotted-Cylinder Based Flutter Exciter, Journal of Aircraft, 2015,52(6):2100-2105.£¨SCI: **030, EI: **400?£©[8] XuHe-yong*, Xing Shi-long, Ye Zheng-yin. Investigation on the UnstructuredRotational Dynamic Overset Grids, AircraftEngineering and Aerospace Technology,2015, 87(4): 293-304. (SCI£º**001£¬EI: **589)[9] XuHe-yong*, Xing Shi-long, Ye Zheng-yin. Numerical Study of the S809 Airfoil AerodynamicPerformance Using a Co-Flow Jet Active Control Concept, Journal of Renewable andSustainable Energy, 2015, 7(2), 023131, pp: 1-20. (SCI£º**031£¬EI: **363)[10] XuHe-yong*, Xing Shi-long, Ye Zheng-yin. Numerical study of ducted-fan lip stallsuppression based on inflatable leading lip cell, ProcediaEngineering, 2015, 126: 158-162.(7th International Conference on FluidMechanics, ICFM7, 24-27 May, Qingdao, 2015) £¨EI: **477£©?[11] XuHe-yong*, Xing Shi-long, Ye Zheng-yin. Numerical simulation of the effect of aco-flow jet on the wind turbine airfoil aerodynamic characteristics,Procedia Engineering, 2015, 126: 706-710. (7th International Conference onFluid Mechanics, ICFM7, 24-27 May, Qingdao, 2015) £¨EI: **382£©?[12]Yang Yun-chao*, Xu He-yong, Wang Jian-lei, Zha Ge-cheng. Large eddy simulationof base drag reduction with jet boat-tail passive flow control,ProcediaEngineering, 2015, 126: 150-157.(7th International Conference on FluidMechanics, ICFM7, 24-27 May, Qingdao, 2015) £¨EI: **522£©?[13] XuHe-yong*, Ye Zheng-yin. Numerical Simulation of Rotor-Airframe AerodynamicInteraction based on Unstructured Dynamic Overset Grids, ScienceChina Technological Sciences, 2012,55(10): 2798-2807. (SCI£º**014£¬EI: **581)[14] XuHe-yong*, Ye Zheng-yin. Numerical Study of Propeller Slipstream based onUnstructured Dynamic Overset Grids, Journal of Aircraft, 2012, 49(2):384-389. (SCI:**004,EI: **831)[15]Xu He-yong*, Ye Zheng-yin. Euler Calculation of Rotor-Airframe InteractionBased on Unstructured Overset Grids, Journal of Aircraft, 2011, 48(2):707-712. (SCI: **036£¬EI: **708)[16]Xu He-yong*, Ye Zheng-yin. Numerical Simulation of Unsteady Flow around ForwardFlight Helicopter with Coaxial Rotors, Chinese Journal of Aeronautics,2011, 24(1): 1-7. (SCI: **001£¬EI: **590)[17] XuHe-yong, Ye Zheng-yin. Investigation of a flutter exciter for aircraft flighttesting using unstructured overset grids. AIAA Paper 2011-6670. AIAAAtmospheric Flight Mechanics Conference, 08-11 August 2011, Portland, Oregon,USA. (EI: **066)[18] XuHe-yong, Ye Zheng-yin. Numerical simulation of rotor-airframe aerodynamicsusing technology of unstructured overset grids. AIAA Paper 2011-6724. AIAAModeling and Simulation Technologies Conference, 08-11 August 2011, Portland,Oregon, USA. (EI: **696)[19] Xu He-yong *, YeZheng-yin. Coaxial Rotor Helicopter in Hover Based on Unstructured DynamicOverset Grids, Journal of Aircraft, 2010, 47(5):1820-1824. (SCI: **037£¬EI: **547)[20]Xu He-yong, Ye Zheng-yin, Wang Gang, Shi Ai-ming. Numerical Simulation ofUnsteady Rotor-Fuselage Aerodynamic Interaction, Acta Aerodynamic Sinica(¿ÕÆø¶¯Á¦Ñ§Ñ§±¨Ó¢ÎÄ)£¬2010£¬28(2): 162-167. (EI: **460)[21]Xu He-yong, Ye Zheng-yin, Wang Gang, Shi Ai-ming. Simulation of HelicopterForward Flight Flow Using Unstructured Overset Grids. AIAA Paper2009-1285, 2009. £¨EI: **702£©[22]Xu He-yong, Ye Zheng-yin, Wang Gang. Unstructured Dynamic Patched Grid Methodand Application. Proceedings of the Sino-Russian Conference on Aerospace Technology.2006£¬Northwestern Polytechnical University, China, pp:291¡«296 (ISBN: 7-5612-2079-0/TH235)ÖÐÎÄÂÛÎÄ·¢±í£¨2011ÄêÒÔÀ´£©£º[1] ÐíºÍÓ£¬ÐÏÊÀÁú£¬Ò¶ÕýÒú£¬ÂíÃ÷Éú. »ùÓÚ³äÆøÇ°Ôµ¼¼ÊõµÄÐýÒíÒíÐͶ¯Ì¬Ê§ËÙÒÖÖÆÑо¿£¬º½¿Õѧ±¨£¬2017£¬38£¨6£©£º120799 £¨EI: **284£©?[2] ËÕÔ˵£¬Ò¶ÕýÒú£¬ÐíºÍÓÂ. ½°¼â¼ä϶ºÍË«½°¼ä¾à¶Ôº­µÀÂÝÐý½°Æø¶¯ÐÔÄܵÄÓ°Ï죬º½¿Õ¶¯Á¦Ñ§±¨?£¬2014£¬29(6):1468-1475. £¨EI: **114£©[3] ÐíºÍÓ£¬Ò¶ÕýÒú. »ùÓڷǽṹǶÌ×Íø¸ñµÄº­µÀÂÝÐý½°ÊýֵģÄ⣬¿ÕÆø¶¯Á¦Ñ§Ñ§±¨£¬2013, 31(3): 306-309.[4] ³Â½Ü£¬Âí´æ±¦£¬ÐíºÍÓÂ. Ò°Õ½»·¾³Ï´óÐÍ·É»ú³¬µÍ¿ÕÆø¶¯ÌØÐÔ·ÖÎö£¬·ÉÐÐÁ¦Ñ§ £¬2013,31(3):217-220,229.[5] ÐíºÍÓ£¬Ò¶ÕýÒú£¬ÕÅΰΰ. »ùÓڷǽṹ×ÔÊÊÓ¦Íø¸ñ¼¼ÊõµÄ¸ß³¬ÉùËÙÁ÷¶¯ÊýֵģÄ⣬¹¤³ÌÁ¦Ñ§£¬2012,29(3):226-229. (EI: **741)[6] ÐíºÍÓ£¬Ò¶ÕýÒú. º­µÀÂÝÐý½°Óë¹ÂÁ¢ÂÝÐý½°Æø¶¯ÌØÐÔµÄÊýֵģÄâ¶Ô±È£¬º½¿Õ¶¯Á¦Ñ§±¨£¬2011£¬26(12): 2820-2825. (EI: **007)[7] ÐíºÍÓ£¬Ò¶ÕýÒú. Èýά·Ç½á¹¹×ÔÊÊÓ¦¶àÖØÍø¸ñ¼¼Êõ£¬¿ÕÆø¶¯Á¦Ñ§Ñ§±¨£¬2011£¬29(3):?229-233. (EI: **604)[8] ÐíºÍÓ£¬Ò¶ÕýÒú. ·Ç½á¹¹Ðýת¶¯Ì¬Ç¶Ì×Íø¸ñ¼¼Êõ¼°ÆäÓ¦Óã¬Î÷±±¹¤Òµ´óѧѧ±¨£¬2011£¬29(2): 171-175. ( EI: **679)ÊÚȨרÀû6Ï[1] ÐíºÍÓ£¬ÐÏÊÀÁú£¬Ñî»ÛÇ¿£¬Çdz¿ÁÁ£¬Ò¶ÕýÒú. Ò»ÖÖº­µÀ·çÉÈ´½¿Ú³äÆøÆøÄÒ¼°ÆäÁ÷¶¯·ÖÀë¿ØÖÆ·½·¨£¬ZL**4.3£¬2018. [2] ÐíºÍÓ£¬ÐÏÊÀÁú£¬Ò¶ÕýÒú. Ò»ÖÖÖ±Éý»úÐýÒí¶¯Ì¬Ê§ËÙÖ÷¶¯Á÷¶¯¿ØÖÆ×°Öã¬ZL**2.2,2016.[3] ÐíºÍÓ£¬Çdz¿ÁÁ£¬Ñî»ÛÇ¿£¬ÐÏÊÀÁú£¬Ò¶ÕýÒú. Ò»ÖÖ¶ÛºóÔµ·çÁ¦»úÒíÐÍ»·Á¿¿ØÖÆ×°Ö㬠ZL**5.9, 2016.[4] ÐíºÍÓ£¬Ñî»ÛÇ¿£¬Çdz¿ÁÁ£¬ÐÏÊÀÁú£¬Ò¶ÕýÒú. ÓÃÓÚÖ±Éý»úÐýÒíҶƬµÄÁªºÏÉäÁ÷¿ØÖÆ×°Ö㬠ZL**7.9,2016.[5] ÐíºÍÓ£¬¶­ÇìÀû£¬¹®ÎÄÐ㣬ҶÕýÒú. »ùÓÚÕûÁ÷ÕÖºÍCoandaÉäÁ÷ЧӦµÄÆû³µÎ²²¿¼õ×è×°Ö㬠ZL**3.1£¬2016.[6] ÐíºÍÓ£¬Ñî»ÛÇ¿£¬Ò¶ÕýÒú. »ùÓÚÁªºÏÉäÁ÷¼¼ÊõµÄ·çÁ¦»úҶƬÁ÷¶¯¿ØÖÆ×°Ö㬠ZL**7.4£¬2017.?¼ÆËã»úÈí¼þÖø×÷Ȩ2Ï[1]µÚÒ»Íê³ÉÈË£¬¡°»ùÓڷǽṹÐýתǶÌ×Íø¸ñµÄ·Ç¶¨³£Á÷¶¯ÊýֵģÄâÈí¼þV1.0¡±£¬±àºÅ£º2016SR195463£¬2016.[2]µÚÒ»Íê³ÉÈË£¬¡°»ùÓÚÔ¼ÊøDelaunay·½·¨µÄ·Ç½á¹¹»ìºÏÍø¸ñÉú³ÉÈí¼þV1.0¡±£¬±àºÅ£º2016SR195576£¬2016.

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