öλÔÓéÀֵǼÈë¿ÚÏÂÔØ

µ¼Ê¦ÐÕÃû£ºº«ÖÒ»ª
ÐÔ±ð£º
ÈËÆøÖ¸Êý£º55

ËùÊôԺУ£ºÎ÷±±¹¤Òµ´óѧ
ËùÊôԺϵ£ºº½¿ÕѧԺ
Ö°³Æ£º½ÌÊÚ
µ¼Ê¦ÀàÐÍ£º
ÕÐÉúöλÔÓéÀֵǼÈë¿ÚÏÂÔØ£ºÁ¦Ñ§


ͨѶ·½Ê½ :
°ì¹«µç»°£º**
µç×ÓÓʼþ£ºhanzh@nwpu.edu.cn


¿ÆÑй¤×÷ :
2003.04 - 2007.10, Î÷±±¹¤Òµ´óѧº½¿ÕѧԺÖú½Ì£¨2003£©£¬½²Ê¦£¨2005£©2007.10 - 2010.09£¬µÂ¹úÓԺ (DLR) ¿ÕÆø¶¯Á¦Ñ§ÓëÁ÷Ìå¼¼ÊõÑо¿ËùÑо¿¿Æѧ¼Ò2010.04?- 2013.04£¬ Î÷±±¹¤Òµ´óѧº½¿ÕѧԺ¸±½ÌÊÚ£¨2010£©2011.11-2013.12£¬Î÷±±¹¤Òµ´óѧº½¿ÕѧԺԺ³¤ÖúÀí2013.04-ÏÖÔÚ£¬Î÷±±¹¤Òµ´óѧº½¿ÕѧԺ½ÌÊÚ£¬2014ÄêÈβ©Ê¿Éúµ¼Ê¦2013.08-2013.09 µÂ¹úÓԺ (DLR) ¿ÕÆø¶¯Á¦Ñ§ÓëÁ÷Ìå¼¼ÊõÑо¿Ëù£¬ÑÇ衹¤Òµ´óѧ¶ÌÆÚ·ÃÎÊ2014.02-2015.01?µÂ¹úÓԺ (DLR) ¿ÕÆø¶¯Á¦Ñ§ÓëÁ÷¶¯¼¼ÊõÑо¿ËùÑо¿¿Æѧ¼Ò·ÃÎʽÌÊÚ2015.02-ÏÖÔÚ Î÷±±¹¤Òµ´óѧº½¿ÕѧԺÁ÷ÌåÁ¦Ñ§Ïµ¸±Ö÷ÈΣ¬º½¿ÕѧԺºÏ×÷·¢Õ¹²¿¸±²¿³¤2017.08-2017.08 Ïã¸Û³ÇÊдóѧ¼ÆËã»ú¿Æѧϵ¶ÌÆÚ·ÃÎÊ Ñо¿·½Ïò1¡¢´úÀíÄ£ÐÍÀíÂÛ¡¢Ëã·¨¼°ÆäÔÚ¹¤³ÌÉè¼ÆÖеÄÓ¦ÓÃ2¡¢·ÉÐÐÆ÷Æø¶¯Óë¶àѧ¿ÆÓÅ»¯Éè¼ÆÀíÂÛÓëËã·¨3¡¢ÒíÐÍ/»úÒí/·çÁ¦»úÉè¼Æ£¬´óÐÍÃñ»úÆø¶¯Éè¼Æ¡¢ÎÞÈË»úÆø¶¯Éè¼Æ4¡¢Ð¸ÅÄÁÙ½ç²ãÁ÷»úÒíÁ÷¶¯»úÀíºÍÓÅ»¯Éè¼Æ5¡¢³¬ÉùËÙ¿Í»úÉù±¬Ô¤²âÓëÓÅ»¯Éè¼Æ6¡¢·ÉÐÐÆ÷ÐÂÐÍÆø¶¯Êý¾Ý¿â¼¼Êõ7¡¢¼ÆËãÁ÷ÌåÁ¦Ñ§Ëã·¨¼°Ó¦Óá¢Ö÷¶¯Á÷¶¯¿ØÖÆ¡¢¼ÆËãÆø¶¯ÉùѧÓëÔëÉùÔ¤²â½ü¼¸Äê·¢±íµÄ´ú±íÐÔ¿ÆÑÐÂÛÎÄ£¨´øÐǺÅΪͨѶ×÷Õߣ©[1] Han, Z. -H., Zhang, Y., Song, C. -X.,Zhang, K. -S., "Weighted Gradient-Enhanced Kriging for High-DimensionalSurrogate Modeling and Design Optimization," AIAA Journal, Vol. 55, No. 12, 2017, pp. 4330-4346.?https://doi.org/10.2514/1.J055842(SCI 2Çø, IF=1.638, º½¿ÕÓ¶¥¼¶ÆÚ¿¯)[2] ?º«ÉÙÇ¿, ËÎÎÄƼ, º«ÖÒ»ª. »ùÓÚÌݶÈÔöÇ¿ÐÍKrigingÄ£Ð͵ÄÆø¶¯·´Éè¼Æ·½·¨Ñо¿, º½¿Õѧ±¨, 2017, 38(7):120817(EI£¬ÖÐÎĶ¥¼¶ÆÚ¿¯)[3] ?º«ÖÒ»ª, ÍõÉÜéª, º«Àò.Ò»ÖÖ»ùÓÚ¶¯Ä£Ì¬·Ö½âµÄÒíÐÍÁ÷¶¯×ªÞæÔ¤²âз½·¨. ¿Õѧ±¨£¬2017, 38(1): 120034 (EI£¬ÖÐÎĶ¥¼¶ÆÚ¿¯) [4]?Liu, J., Song, W. -P., Han, Z. -H., andZhang, Y., ¡°Efficient Aerodynamic Shape Optimization of Transonic Wings Using aParallel Infilling Strategy and Surrogate Models,¡± Structural andMultidisciplinary Optimization, Vol. 55, No. 3, 2016, pp. Çø£¬IF=2.377,±¾ÈËΪͨѶ×÷Õß)[5]?Han,Z. -H., Song, W. -P., Gao, Y. -W., ¡°Design and Verification of Airfoil Familiesfor Large-Size Wind Turbine Blades,¡± Applied Mathematics and Mechanics (EnglishEdition),2016, 37: 67-84[6]?º«ÖÒ»ª, KrigingÄ£Ðͼ°´úÀíÓÅ»¯Ëã·¨Ñо¿Ð½øÕ¹£¬º½¿Õѧ±¨£¬2016, 37(11):3197-3225 (EI£¬ÖÐÎĶ¥¼¶ÆÚ¿¯)[7]?Han, Z. -H., and Goertz, S, ¡°A HierarchicalKriging Model for Variable-Fidelity Surrogate Modeling¡±, AIAA Journal, Vol.50,No. 9, September, pp.1885-1896. DOI:10.2514/1.J051354 (SCI 2Çø£¬IF=1.638, º½¿ÕÓ¶¥¼¶ÆÚ¿¯)[8]?Han, Z. -H., Zimmermann, R., and Goertz,S., ¡°An Alternative Cokriging Model for Variable-Fidelity Surrogate Modeling,¡±AIAA Journal£¬Vol. 50, No.5, 2012, pp.1205-1210.doi: 10.2514/1.J051243 (SCI 2Çø£¬IF=1.638, º½¿ÕÓ¶¥¼¶ÆÚ¿¯)[9]?Han, Z. -H., Goertz, S., and Zimmermann,R., ¡°Improving Variable-Fidelity Surrogate Modeling via Gradient-EnhancedKriging and a Generalized Hybrid Bridge Function,¡± Aerospace Science andTechnology, Vol.25, No.1, 2013, pp.177-189 doi:10.1016/j.ast.2012.01.006,2012. £¨SCI 2Çø£¬IF=2.057£©[10]?º«ÖÒ»ª, ËÎÎÄƼ, ¸ßÓÀÎÀ. ´óÐÍ·çÁ¦»úÒíÐÍ×åµÄÉè¼ÆÓëʵÑé. Ó¦ÓÃÊýѧÓëÁ¦Ñ§£¬2013[11]?Han, Z. -H., Zhang, K. -S., Song, W. -P.,and Qiao, Z. -D., "Optimization of Active Flow Control over an Airfoil Usinga Surrogate-Management Framework", Journal of Aircraft, 2010, Vol. 47, No.2, pp. 603-612. EI: **586, SCI : **024 doi: 10.2514/1.45899 £¨SCI 4Çø£©[12]?Han, Z.-H, He, F. Song, W. -P. and Qiao, Z.-D., ¡°A Preconditioned Multigrid Method for Efficient Simulation ofThree-Dimensional Compressible and Incompressible Flows£¬¡± Chinese Journal of Aeronautics£¬Vol.20, No.4, 2007. pp.289-296 (SCI£º**001 EI-**570).£¨SCI 4Çø£©[13]?Wu , M. -M., Han, Z. -H., Wang, S. -N.,Song, W. -P., and Esteban, F., ¡°A DMD-Based Automatic Transition PredictionMethod for Flows over Airfoils,¡± AIAA 2017-4303, 2017[14]?Zhang, Y., Han, Z. -H., Leifsson, L. -T.,¡°Surrogate-Based Optimization Applied to Benchmark Aerodynamic DesignProblems,¡± AIAA 2017-4367, 2017[15]?Han, Z. -H., ¡°SurroOpt: A GenericSurrogate-based Optimization Code for Aerodynamic and MultidisciplinaryDesign,¡± 30th Congress of the International Council of the AeronauticalSciences, ICAS 2016. [16]?Han Z. -H., Song C. -X., and Zhang Y. ¡°ANew Formulation of Gradient-Enhanced Surrogate Model and Application toAerodynamic Design,¡± AIAA 2016-3869, 2016[17]?Zhang, Y., Han, Z.-H., Shi, L.-X.,¡°Multi-Round Surrogate-Based Optimization for Benchmark Aerodynamic DesignProblems,¡± AIAA 2016-1545, 2016, 54th AIAA Aerospace Sciences Meeting, SanDiego, 2016.1.4-2016.1.8. [18]?Shi, L.-X., Han, Z.-H., Shahbaz, M.,¡°Surrogate-Based Robust Airfoil Design under Aleatory Operating Conditions andGeometric Uncertainties,¡± AIAA 2016-0810, 2016, 54th AIAA Aerospace SciencesMeeting, San Diego, 2016.1.4-2016.1.8. רÖøÕ½Ú[1] Han, Z. -H., Zhang, K. -S, ¡°Surrogate BasedOptimization,¡± Intec Book, Real-world Application of Genetic Algorithm, 2012,pp.343-362[2]?ËïÇØ£¬º«ÖÒ»ª£¬ÖÓСƽ£¬·É»úÔغÉÓë»ú¹¹²¼¾Ö£¨ÒëÖø£©£¬Öк½³ö°æ´«Ã½ÓÐÏÞÔðÈι«Ë¾£¬2014½ü¼¸ÄêÖ÷³ÖºÍ²Î¼ÓµÄ¿ÆÑÐÏîÄ¿1¡¢·ÉÐÐÆ÷¶àÄ¿±êñîºÏÆø¶¯ÓÅ»¯Éè¼Æ¼¼Êõ£¬¹ú¼Ò¡°Ê®ÈýÎ塱װ±¸Ô¤Ñй²Óü¼Êõ£¨¹ú¼Ò¼¶ÏîÄ¿£©£¬×ܾ­·Ñ420Íò£¬2017.08-2020.12£¬±¾ÈËΪÏîÄ¿¸ºÔðÈË£»2¡¢»ùÓÚ¶à²ãÌݶÈÔöÇ¿KrigingÄ£Ð͵ĸßάȫ¾ÖÆø¶¯ÓÅ»¯Éè¼Æ·½·¨£¬¹ú¼Ò×ÔÈ»¿Æѧ»ù½ðÃæÉÏÏîÄ¿£¨¹ú¼Ò¼¶ÏîÄ¿£©£¬Ö±½Ó¾­·Ñ62Íò£¬2018.01-2020.12£¬±¾ÈËΪÏîÄ¿¸ºÔðÈË£»3¡¢Ç°ÂÓ²ãÁ÷»úÒíµÄ¼õ×è»úÀíÓëÓÅ»¯Éè¼Æ·½·¨Ñо¿£¬º½¿Õ¿Æѧ»ù½ðÏîÄ¿£¨Ê¡²¿¼¶ÏîÄ¿£©£¬12Íò£¬2017.9-2018.10£¬±¾ÈËΪÏîÄ¿¸ºÔðÈË£»4¡¢XXÇ°ÂÓ²ãÁ÷»úÒíµÄ»úÀí·ÖÎöÓëÓÅ»¯Éè¼Æ£¬¹ú¼ÒÊ®ÈýÎåÔ¤ÑÐÖصãʵÑéÊÒ»ù½ðÏîÄ¿£¨Ê¡²¿¼¶ÏîÄ¿£©£¬30Íò£¬2017.08-2019.09, ±¾ÈËΪÏîÄ¿¸ºÔðÈË£»5¡¢Ãñ»úCFDÇ°Ñؼ¼Êõ-ÏȽøתÞæÄ£ÐÍ£¬¹¤ÐŲ¿Ä³×¨Ï¹ú¼Ò¼¶ÏîÄ¿£©£¬2016.01-2018.12, ×ܾ­·Ñ1000Íò£¨±¾È˸ºÔðµÚ3רÌ⣬¾­·Ñ130Íò£©.6¡¢Ä³·ÉÐÐÆ÷ÒíÐͼ°»úÒíÍâÐÎÉè¼Æ, º½ÌìÈýԺίÍÐÏîÄ¿£¨ºáÏò¿ÎÌ⣩,22Íò£¬2015.01-2016.12£¬±¾ÈËΪÏîÄ¿¸ºÔðÈË£»7¡¢»ùÓڸĽøco-KrigingÄ£Ð͵ĸßάÆø¶¯ÓÅ»¯Éè¼Æз½·¨Ñо¿£¬¹ú¼Ò×ÔÈ»¿Æѧ»ù½ðÃæÉÏÏîÄ¿£¨¹ú¼Ò¼¶ÏîÄ¿£©£¬80Íò£¬2013.01-2016.12, ±¾ÈËΪÏîÄ¿¸ºÔðÈË8¡¢ÏȽø·çÁ¦»úÒíÐÍ×åÉè¼Æ¼¼ÊõÑо¿£¬¹ú¼Ò¸ß¼¼Êõ·¢Õ¹¼Æ»®£¨863£©£¨¹ú¼Ò¼¶ÏîÄ¿£©£¬×ܾ­·Ñ678Íò£¬ 2012.01-2015.12£¬±¾ÈËΪ¹²Í¬Ö÷³ÖÈË9¡¢ÒíÐÍXXÆ×ϵÓëÊý¾Ý¿â£¬Ô­×Ü×°¡°Ê®¶þÎ塱Æø¶¯Ô¤ÑУ¨¹ú¼Ò¼¶ÏîÄ¿£©£¬×ܾ­·Ñ2000Íò£¨±¾È˾­·Ñ80Íò£©£¬2014.10-2015.12, ±¾ÈËΪµÚËÄרÌ⸺ÔðÈË10¡¢XXÒí¶æÉè¼Æ¹æÂÉÓëÊý¾Ý¼¯Èí¼þÉè¼Æ¹¦ÄÜ¿ª·¢£¬¹ú¼Ò¿Æ¼¼ÖØ´óרÏî×ÓÏîÄ¿£¬65Íò£¬2015.01-2015.12£¬±¾ÈËΪÏîÄ¿¸ºÔðÈË11¡¢ñîºÏתÞæ×Ô¶¯Åж¨µÄXX»úÒí¸ß¾«¶ÈÆø¶¯¼ÆËã·½·¨Óë¸ßЧÓÅ»¯Éè¼Æ¼¼ÊõÑо¿£¬¹ú¼Ò¡°Ê®¶þÎ塱¿ÕÆø¶¯Á¦Ñ§Ô¤ÑУ¬70Íò£¬2011.01-2015£®12£¬±¾ÈËΪ¹²Í¬Ö÷³ÖÈË12¡¢Ò»ÖÖÊÊÓÃÓÚ¸ßάÎÊÌâµÄco-Kriging´úÀíÄ£ÐÍз½·¨Ñо¿£¬¹ú¼Ò×ÔÈ»¿Æѧ»ù½ðÇàÄê»ù½ð£¬22Íò£¬2010.01-2012.12£¬±¾ÈËΪÏîÄ¿¸ºÔðÈË13¡¢»ùÓÚÌݶÈÔöÇ¿µÄKrigingÄ£Ð͵ÄÆø¶¯ÓÅ»¯Éè¼Æз½·¨£¬º½¿Õ¿Æѧ»ù½ð£¬10Íò£¬2011.10 -2013.09£¬±¾ÈËΪÏîÄ¿¸ºÔðÈË14¡¢ÒíÐÍXXÈÆÁ÷ÌØÐÔÑо¿£¬¹ú¼Ò¿Æ¼¼ÖØ´óרÏî×Ó¿ÎÌ⣬70Íò£¬2012.01-2012.12£¬±¾ÈËΪ¹²Í¬Ö÷³ÖÈË15¡¢ÃæÏòC919ÔöÉý×°ÖÃÓÅ»¯µÄ´úÀíÄ£ÐÍÈí¼þ¿ª·¢£¬¹ú¼Ò¿Æ¼¼ÖØ´óרÏî×Ó¿ÎÌ⣬ÖйúÉÌ·É£¬18Íò£¬2011.09-2012.12£¬±¾ÈËΪÏîÄ¿¸ºÔðÈ˹ú¼Ò·¢Ã÷רÀû1¡¢¼æ¹Ë¿çÉùËٺ͸߳¬ÉùËÙÆø¶¯ÌØÐÔµÄиÅÄîÒíÐÍ£¬¹ú¼Ò·¢Ã÷רÀû£¬ZL**9.1, 2017,±¾ÈËΪµÚÒ»·¢Ã÷ÈË£»2¡¢Ò»Öָ߿յÍËÙ×ÔÈ»²ãÁ÷¸ßÉýÁ¦ÒíÐÍ£¬¹ú¼Ò·¢Ã÷רÀû£¬ZL**3.9£¬,±¾ÈËΪµÚÒ»·¢Ã÷ÈË£»3¡¢Ò»ÖÖÊÊÓÃÓÚÕ×Íß¼¶·çÁ¦»úҶƬµÄ30%ºñ¶ÈÒíÐÍ£¬¹ú¼Ò·¢Ã÷רÀû£¬ZL**0.2,±¾ÈËΪµÚÒ»·¢Ã÷ÈË£»4¡¢Ò»ÖÖÓÃÓÚÕ×Íß¼¶·çÁ¦µÄ25%ºñ¶ÈÖ÷ÒíÐÍ£¬£¬¹ú¼Ò·¢Ã÷רÀû£¬ZL**1.7,±¾ÈËΪµÚÒ»·¢Ã÷ÈË£»5¡¢Ò»ÖÖÓÃÓÚÕ×Íß¼¶·çÁ¦»úҶƬµÄ21%ºñ¶ÈÖ÷ÒíÐÍ£¬¹ú¼Ò·¢Ã÷רÀû£¬ZL**2.8,±¾ÈËΪµÚÒ»·¢Ã÷ÈË£»6¡¢Ò»×åÓÃÓÚÕ×Íß¼¶·çÁ¦»úҶƬµÄÒíÐÍ£¬¹ú¼Ò·¢Ã÷רÀû£¬ZL**5.1£¬2011,±¾ÈËÅÅÃûµÚ8Èí¼þÖø×÷Ȩ1¡¢SurroOpt»ùÓÚ´úÀíÄ£Ð͵ĶàÄ¿±ê¶àÔ¼Êø¸ßЧͨÓÃÓÅ»¯Èí¼þ£¬2013SR029744£¬º«ÖÒ»ª£¬Áõ¿¡£¬ËÎÎÄƼ2¡¢¸ß³¬ÉùËÙÒíÃæ¶æÃæÊý¾Ý¿âÈí¼þ¡¢2016SR161170£¬º«ÖÒ»ª, ¸»å·£¬ÁõÃô3¡¢PMNS3DñîºÏ±ß½ç²ãתÞæ×Ô¶¯Ô¤²âµÄRANS·½·¨¼ÆËãÈí¼þ£¬2017SR272784º«ÖÒ»ª£¬Ðí½¨»ª£¬ËÎÎÄƼ4¡¢ROTNSÐýתҶƬÆø¶¯·ÖÎöÈí¼þ£¬2017SR292783£¬Ðí½¨»ª£¬º«ÖÒ»ª¡¢ËÎÎÄƼ

½ÌÓý±³¾° :
1996.09 - 2000.07£¬Î÷±±¹¤Òµ´óѧ·É»úϵ¿ÕÆø¶¯Á¦Ñ§Óë·ÉÐÐÁ¦Ñ§öλÔÓéÀֵǼÈë¿ÚÏÂÔØѧʿѧλ2000.07 - 2003.04£¬Î÷±±¹¤Òµ´óѧº½¿ÕѧԺÁ÷ÌåÁ¦Ñ§öλÔÓéÀֵǼÈë¿ÚÏÂÔØ˶ʿѧλ2003.04 - 2007.07£¬Î÷±±¹¤Òµ´óѧº½¿ÕѧԺÁ÷ÌåÁ¦Ñ§öλÔÓéÀֵǼÈë¿ÚÏÂÔز©Ê¿Ñ§Î»