梁珂


的个人主页 http://teacher.nwpu.edu.cn/liangke

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基本信息 The basic information

梁珂

航空学院

博士研究生毕业

博士

副教授

航空宇航科学-飞行器设计

k.liang@nwpu.edu.cn

18392957817

工作经历 Work Experience

  • 副教授,    2016/11-今,              航空学院, 西北工业大学

  • 兼职研究员,2017/01-今,             钱学森空间技术实验室,中国空间技术研究院

  • 副研究员,  2015/04-2016/11,   钱学森实验室,中国空间技术研究院

  • 博士后,    2013/07-2015/02,   代尔夫特理工大学,航空宇航学院,荷兰

教育经历 Education Experience

· 博士学位(2010/10-2013/07: 代尔夫特理工大学,航空宇航学院,荷兰

  专业:航空宇航结构设计与计算力学专业

· 博士学位(2007/09-2012/11: 西北工业大学,航空学院,中国.

  专业:飞行器设计

· 学士学位(2003/09-2007/06: 西北工业大学,航空学院,中国.

  专业:飞行器设计

荣誉获奖 Awards Information

·           2015/03  欧盟FP7项目DESICOS杰出贡献奖(Excellent Work),德国宇航中心DLR颁发

科学研究 Scientific Research

1. 国家自然科学基金青年基金(11602286),薄壁结构静、动力屈曲分析的新型非线性有限元降阶方法研究,2017/01-2019/12,27万元,在研,主持

2. 陕西省自然科学基金(2018JQ1071),复合材料加筋壁板后屈曲强度分析的非线性有限元全程降阶方法研究,2018/1-2019/12, 3万元,在研,主持

3. 航天科学技术基金,变刚度复合材料结构极限承载的非线性有限元降阶方法研究,2018/1-2018/12, 8万元,在研,主持

4. 航天一院高校联合创新基金(CALT基金)(2017MC010110),轴压大型薄壁筒壳屈曲承载力的高效可靠评估,2017/08-2018/08,10万元,在研,主持

5. 中央高校基本科研业务基金(G2017KY0302),复合材料加筋壁板后屈曲强度分析,2017/01-2018/12,20万元,在研,主持

6. 钱学森空间技术实验室自主研发课题(m-2015-hb-kh),航天薄壁结构屈曲承载能力的高效高精度、鲁棒评估方法研究,2015/04-2016/11,20万元,结题,主持

7. 欧盟7框架项目DESICOS:航空宇航工程中大型复合材料圆柱壳结构的屈曲稳定性设计,7th Framework European Program (No. 282522) 2012/03-2015/07,300万欧元,参与

8. 航天复材-金属连接件的强度分析, 由荷兰宇航局Dutch Space资助,2011/06-2012/02,参与 

学术成果 Academic Achievements

英文出版物

Ke Liang, A Koiter-Newton arc-length method for buckling sensitive structures. PhD thesis, Printed by: Wohrmann Print Service, the Netherlands. 2013. ISBN 978-94-6203-387-0. 205 pages

期刊论文(中科院分区)

1. Ke Liang, et. al. A Koiter-Newton approach for nonlinear structural analysis. International Journal for numerical method in Engineering. 2013, 96(12): 763-786. 二区

2. Ke Liang, et. al. The Koiter-Newton approach using von Karman kinematics for buckling analyses of imperfection sensitive structures. Computer Method in Applied Mechanics and Engineering. 2014, 279: 440-468.  一区

3. Ke Liang, et. al. A new robust design for imperfection sensitive stiffened cylinders used in aerospace engineering. Science China Technological Sciences. 2015,58:1-7. 三区

4. Ke Liang, et. al. An eigenanalysis-based bifurcation indicator proposed in the framework of a reduced-order modeling technique for nonlinear analysis. International Journal of Non-linear Mechanics. 2016, 81: 129-138. 三区 

5. Ke Liang, et. al. Co-rotational finite element formulation used in the Koiter-Newton method for nonlinear buckling analyses. Finite Elements in Analysis and Design.2016,116:38-54. 二区

6. Ke Liang, et. al. Nonlinear buckling analysis of the conical and cylindrical shells using the SGL strain based reduced order model and the PHC method. Aerospace Science and Technique. 2016, 55:103-110. 二区

7. Ke Liang. A global-local finite element analysis of hybrid composite-to-metal bolted connections used in aerospace engineering. Journal of Central South University. 2017, 24(6): 1225-1232.四区

8. Ke Liang. Koiter-Newton analysis of thick and thin laminated composite plates using a robust shell element. Composite Structures, 2017, 161:530-539.  二区  

 9. Ke Liang, et. al. Buckling and post-buckling analysis of the delaminated composite plates using the Koiter–Newton method, Composite Structures, 2017, 168266-276二区

10. Ke Liang, et. al. Reduced-order modeling analysis of shell structures buckling using a co-rotational solid-shell element. Aerospace Science and Technology. In press, 2017, 70:435-444.  二区 

11. Ke Liang, et. al. A modified Newton-type Koiter-Newton method for tracing the geometrically nonlinear response of structures.  International Journal for numerical method in Engineering. 2017. 2018. 113(10): 1541-1560. 二区

12. Ke Liang, et. al. Koiter's reduction finite element method for nonlinear stability analysis of thin-walled structures. International Journal of Computational Methods. 2018. 15(3): 1843004-1-16. 三区

13. Ke Liang, et. al. Investigation on imperfection sensitivity of composite cylindrical shells using the nonlinearity reduction technique and the polynomial chaos method. Acta Astronautica. 2018. 146: 349-358. 二区

14. Ke Liang, et. al. Nonlinear buckling analysis of variable stiffness composite plates based on the reduced order model, Composite Structures, 2018, 206681-692. 二区

非一作:

  1. C. Yang, Z. Lu, Z. Yang, K. Liang. Parameter identification for structural dynamics based on interval analysis algorithm. Acta Astronautica. 2018. 145: 131-140.

  2. Q. Sun, X. R. Liu, K. Liang. Impact fatigue life prediction for notched specimen of steel aermet100 subjected to high strain rate loading. International Journal of Applied Mechanics. 2018. 10(03): 1-18.

  3. D. Magisano, Ke Liang, et al. An efficient mixed variational reduced order model formulation for non-linear analyses of elastic shells. International Journal for numerical method in Engineering. 2018, 113: 634-655. 二区

  4. L. Friedrich, S. Loosen, Ke Liang, et al. Stacking sequence influence on imperfection sensitivity of cylindrical composite shells under axial compression. Composite Structures. 2015, 134:750-761. 二区

  5. P. Q. He, Q. Sun, K. Liang. Generalized modal element method: Part-I: Theory and its application to eight-node unsymmetric and symmetric solid elements. Computational Mechanics. 2018, accepted.

  6. P. Q. He, Q. Sun, K. Liang. Generalized Modal element method: part II- Applications to eight-node unsymmetric and symmetric solid-shell elements. Computational Mechanics. 2017, accepted.


专利

1. 发明专利(201510737131.2):一种高效高精度地探测及跟踪结构屈曲分支路径的方法,第一发明人 

2. 发明专利(201610072681.1):一种轴压筒壳结构承载力折减系数及其确定方法,第一发明人

3. 发明专利(201710604375.2):完全基于降阶模型的结构非线性屈曲平衡路径跟踪方法,第一发明人

综合介绍 General Introduction

研究领域

· 薄壁结构屈曲分析与设计,复合材料失效分析,飞行器结构优化设计

· 结构计算力学:非线性摄动降阶法,有限单元法