【人物简介】

　　谢宗蕻，男，满族，1973年3月生,湖南湘潭人。 　　1991年保送到南京航空航天大学飞行器设计专业,1995年获飞行器设计专业学士学位,1998年获飞行器设计专业硕士学位,1999年赴美国马里兰大学航空航天工程系留学,2002年获航空航天工程专业科学硕士学位,2003年获航空航天工程专业哲学博士学位。2004年被聘为西北工业大学航天学院飞行器设计专业副教授，2009年破格晋升为教授，2011年晋升为博士生导师。 　　目前为中国复合材料学会理事、中国宇航学会结构与环境工程专业委员会委员、科技部国际科技合作项目评审专家。

【研究方向】

主要研究方向为飞行器设计、结构力学和复合材料。多年来从事飞行器结构，尤其是复合材料结构的设计、分析、制造、测试及维修等方面的研究，曾承担了几十项基金及横向课题研究工作。

【研究成果】

主要学术成就 1. Xie, Z. and Vizzini A. J., “On Residual Compressive Strength Prediction of Composite Sandwich Panels after Low-velocity Impact Damage,” Acta Mechanica Solida Sinica, Vol. 19, No. 1, March 2006, pp.9-17（SCI：000237838200002） 2. Xie, Z. and Vizzini A. J., “Damage Propagation of a Composite Sandwich Panel Subject to Increasing Uniaxial Compression after a Low-Velocity Impact,” Journal of Sandwich Structures & Materials, Vol.7, No.4, July 2005, pp.269-288（SCI：000230140400001） 3. Xie, Z. and Vizzini A.J., “A Feasible Methodology For Engineering Applications In Damage Tolerance of Composite Sandwich Structures”, Journal of Composite Materials, Vol. 38/11, June 2004, pp.891-914（SCI：000222365300001 & EI：2004278246653）

【科研项目】

多年来从事飞行器结构，尤其是复合材料结构的设计、分析、制造、测试及维修等方面的研究，曾承担了几十项基金及横向课题研究工作。

【论文著作】

学报: 1) Xie, Z.H., Yan, Q. and Li, X., "Investigation on low velocity impact on a foam core composite sandwich panel ", International Journal of Steel and Composite Structures, 2014, 17(2): 159-172. (SCI:000344975400003; EI:20143618129022) 2) Xie, Z.H., Peng, F. and Zhao, T., "Experimental study on fatigue crack propagation of fiber metal laminates ", International Journal of Steel and Composite Structures, 2014, 17(2): 145-157. (SCI:000344975400002; EI:20143618129021) 3)谢宗蕻,刘海涵,田江.复合材料泡沫夹层板准静态压痕实验的有限元模拟[J].材料工程,2014,2:13-17.(EI:20141217481678) 4) Xie Zonghong, Sun Junfeng, Li Wei, Zhao Jian, Yue, Xishan, “Study on the equivalent thermal conductivity of superalloy honeycomb core structures”, Applied Mechanics and Materials, Vol.483, 2014, pp.194-198(EI:20140317210751, ISTP: 000335714400042) 5) Xie Zonghong, Peng Fei, Zhang Peng, Zhao Wei, “A smart skin antenna structure for global navigation satellite system”, Applied Mechanics and Materials, Vol.464, 2014, pp.316-320(EI:20140317210751, ISTP:000336635500057) 6) Xie Zonghong, Yan Qun, “Numerical modeling on low velocity impact on a foam core sandwich panel”, Applied Mechanics and Materials, Vol.527, 2014, pp.53-56 (EI:20141017436728) 7)谢宗蕻,刘海涵.层间增韧复合材料层合板低速冲击损伤预测[J].南京航空航天大学学报,2013,45:686-692. 8) Xie Zonghong, Liu Haihan, Zhao Jian, Sun Junfeng, Peng Fei, Sui Xiaodong, “Experimental study on interlaminar shear properties of T300/BMI composite laminates”, Adv. Mater. Res., Vol.718-720, 2013, pp.157-161（EI：20133516682939） 9) Xie Zonghong, Liu Xiaoyu, Yue Xishan, Yan Qun, Sun Junfeng, Jing Yongjuan, “Out-of-plane mechanical property test on titanium honeycomb cores”, Adv. Mater. Res., Vol.718-720, 2013, pp.1018-1023（EI：20133516683096） 10) Xie Zonghong, Yan Qun, Tian Jiang, Liu Xiaoyu, “Quasi-static indentation test on composite sandwich panels with foam core”, Adv. Mater. Res., Vol.718-720, 2013, pp.214-218（EI：20133516682949） 11) Xie Zonghong, Li Xiang, Zhao Jian, Hao Jie, Sun Yanpeng, Sui Xiaodong, “Study on the Mode I interlaminar fracture toughness of multi-directional composite laminates”, Adv. Mater. Res., Vol.718-720, 2013, pp.186-190（EI：20133516682944） 12) Xie Zonghong, Kong Xiangdong, Yan Qun, Zhao Jian, Liu Xiaoyu, Jiang Ye, “Test on composite stiffened panel with different stringer cut-outs under uniaxial tension”, Adv. Mater. Res., Vol.718-720, 2013, pp.1055-1059（EI：20133516683103） 13) Wang Hongqing, Yan Qun, Xie Zonghong, Sui Xiaodong, “Modeling and Experimental Validation of Composite Stiffened Panels under Uniaxial Tension”, Adv. Mater. Res., Vol.791, 2013, pp.415-418(EI:20134516955304) 14) Jing Yongjuan., Li Xiaohong, Xie Zonghong, Yue Xishan, “Influence of geometrical parameters on specific strength of Ti-based alloy honeycomb unit”, Transactions of China Welding Institution, Vol.34, 2013, pp.103-106 (in Chinese, EI:20134616974447) 15) Xie Zonghong, Zhao Tianjiao and Wu Rui, “Experimental Study on Fatigue Crack Propagation of Glare3-3/2 with Mechanics Properties”, Adv. Mater. Res., Vol.600, Oct. 2012, pp.273-278 (in English，EI:20125115821136, ISTP: 000317630300061) 16) Xie Zonghong, Tian Jiang, etc., “Study on the Residual Compressive Strength of a Composite Sandwich Panel with Foam Core after Low Velocity Impact”, Adv. Mater. Res., Vol.430-432, Jan. 2012, pp.484-487 (in English, EI:20120414713599, ISTP: 000310495400108) 17) Xie Zonghong, Zhao Wei, etc., “The Development of a Multi-functional Composite Embedded Smart-skin Antenna Structure”, Adv. Mater. Res., Vol.484-487, 2012, pp.2743-2747. (in English, EI:20121414924139，ISTP：000312926101158) 18)赵剑,谢宗蕻,李玮,田江.耐热合金蜂窝等效导热率的实验研究[J].固体火箭技术,2011,34(4):529-532.(EI: 20114214431779) 19)谢宗蕻,张磊,苏霓.离位增韧复合材料层合板准静态压入实验研究[J].材料工程,2011,1:42-46.(EI: 20111113746950) 20)李玮,谢宗蕻,赵剑.蜂窝芯体面外方向导热系数等效研究[J].真空与低温, 2010,16(3):162-166. 21)谢宗蕻,苏霓,张磊.复合材料蜂窝夹芯板低速冲击损伤扩展特性[J].南京航空航天大学学报,2009, 41(1):30-35 (EI:20091412008495) 22)谢宗蕻,赵剑.高温合金热防护系统设计与分析[J].宇航学报,2008,29(5):1677-1683. (EI:20085111797859) 23)谢宗蕻,李磊,赵剑.空间智能天线夹芯结构热变形力学分析[J].南京航空航天大学学报,2008,40(5): 617-621.(EI:20084711720583) 24)赵剑，谢宗蕻等.蜂窝芯体材料面外等效弹性模量预测与分析[J].航空材料学报,2008,28(4):94-100(EI:20083711540902) 25) Xie, Z.H. and Vizzini A. J., “On Residual Compressive Strength Prediction of Composite Sandwich Panels after Low-velocity Impact Damage”, Acta Mechanica Solida Sinica, Vol.19/1, 2006, pp.9-17 (in English，SCI：000237838200002) 26) Xie, Z.H. and Vizzini A. J., “Damage Propagation of a Composite Sandwich Panel Subject to Increasing Uniaxial Compression after a Low-Velocity Impact”, Journal of Sandwich Structures & Materials, Vol.7, No.4, July 2005, pp.269-288 (in English，SCI：000230140400001) 27) Xie, Z.H. and Vizzini A.J., “A Feasible Methodology For Engineering Applications In Damage Tolerance of Composite Sandwich Structures”, Journal of Composite Materials, Vol. 38/11, June 2004, pp.891-914 (in English，SCI：000222365300001) 28)谢宗蕻.蜂窝夹芯结构雷达罩鸟撞有限元分析与模拟[J].爆炸与冲击,1999,19(3):235-242.(EI:2000215121490) 29)谢宗蕻,乔新.分布式交互仿真技术的理论与实现[J].南京航空航天大学学报,1998, 30. 国际会议: 1) Peng, F., Xie, Z.H., “The study about the effect of geometric parameters’ and material properties’ changing on the electromagnetic performance of BSSAS”, 4th International Conference on Applied Mechanics and Mechanical Engineering, Singapore, Singapore, Oct. 2013, Vol.459, pp.76-81. (ISTP:000336693100013) 2) Li, X., Xie, Z.H. and Bao, P.P. etc., “Ballistic Impact Behavior of Composite Laminates”, World Congress on Engineering and Technology, Shanghai, China, Oct. 2011, Vol.4, pp.299-302. 3) Xie, Z.H., Tian, J. and Zhao, J. etc., “Study on the damage propagation of a composite sandwich panel with foam core after low velocity impact”, Proceedings of the 18th International Conference of Composite Materials (ICCM18), Jeju, Korea, August 2011 (EI:20131516201298) 4) Zhao, J., Xie, Z.H., and Li, L. etc, “On Effective Thermal Conductivity of Super Alloy Honeycomb Core in Sandwich Structures”, Proceedings of the 18th International Conference of Composite Materials (ICCM18), Jeju, Korea, August 2011 (EI:20131516201521) 5) Xie, Z.H., Zhao, W. and Li, L., “The Development of a Multifunctional Embedded Composite Smart Skin Antenna Structure”, Proceedings of the 18th International Conference of Composite Materials (ICCM18), Jeju, Korea, August 2011 (EI:20131516201451) 6) Xie, Z.H., Li, W. and Zhao, J. “Study on the out-of-plane shear properties of superalloy honeycomb cores”, Proceedings of the 18th International Conference of Composite Materials (ICCM18), Jeju, Korea, August 2011 (EI:20131516201566) 7) Xie, Z.H., Li, X. and Bao, P.P., “Low Velocity Impact Damage Characteristics of Interlayer Toughened Composite Laminates”, Proceedings of the 18th International Conference of Composite Materials (ICCM18), Jeju, Korea, August 2011 (EI:20131516201185) 8) Xie, Z.H., Bi, R.B. and Zhang, L., “Damage Prediction of A Composite Laminate Under Quasi-Static Indentation Force”, Proceedings of the 2nd International Conference on Computer Engineering and Technology (ICCET 2010), Chengdu, China, April 2010, Vol.5, pp.561-564. (EI:20104313317300) 9) Zhao, J. and Xie, Z.H., “Parametric Study on Buckling Behavior of Composite Hat-Stiffened Panels under Uniaxial Compression”, Proceedings of the 2nd International Conference on Computer Engineering and Technology (ICCET 2010), Chengdu, China, April 2010, Vol.5, pp.565-568. (EI:20104313317301) 10) Xie, Z.H. and Vizzini, A. J., “On Residual Compressive Strength Prediction of Composite Sandwich Panels after Low-velocity Impact Damage”, Proceedings of the 7th International Conference on Sandwich Structures (ICSS-7), Aalborg University, Aalborg, Denmark, Aug. 2005, pp.363-372. 11) Xie, Z.H. and Vizzini, A.J., “A Feasible Methodology For Engineering Applications In Damage Tolerance of Composite Sandwich Structures”, International SAMPE Symposium in Long Beach, CA, USA May 2003 12) Xie, Z.H. and Vizzini, A.J., “A Modified Analytical Model for the Prediction of The Damage Propagation of a low-velocity Impacted Sandwich Panel under Compression”, Proceedings of the 17th annual technical conference of American Society for Composites, West Lafayette, IN, USA, October 2002 (Winner of Best Paper in 1st place) 13) Xie, Z.H. and Vizzini, A.J., “The Presence of a Delamination in Damage Growth of an Impacted Sandwich Panel”, Proceedings of the 16th annual technical conference of American Society for Composites, Blacksburg, VA, USA, September 2001