宋智广部门：航天与建筑工程学院

学科：力学

职务：

职称：教授

指导
资格：博士生导师
硕士生导师
电话：**

传真：

邮箱：z.g.song@hrbeu.edu.cn

邮编：150001

地址：哈尔滨市南岗区南通大街145号哈尔滨工程大学三乙实验楼201室
个人简介
Dr. Zhiguang SONG, Sept. 1986
Full Professor, Humboldt Research Fellow
College of Aerospace and Civil Engineering
Harbin Engineering University, Harbin, 150001, P.R. China
Research interests: Aerothermoelasticity; Structural Vibration and Control; Nonlinear Dynamics; Computational Mechanics
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宋智广，教授，博导，德国洪堡学者，1986年9月出生于辽宁抚顺。

教育经历
Education
2011/09–2014/10, Ph.D, General and Fundamental Mechanics, Harbin Institute of Technology
2009/09-2011/07, M.Sc, General and Fundamental Mechanics, Harbin Institute of Technology
2005/09-2009/07, B.Sc, Engineering Mechanics, Harbin University of Science and Technology
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2011/09–2014/10，哈尔滨工业大学，一般力学与力学基础，工学博士
2009/09-2011/07，哈尔滨工业大学，一般力学与力学基础，工学硕士
2005/09-2009/07，哈尔滨理工大学，工程力学，工学学士




工作经历
Employment history
2018/04-Present, Professor, College of Aerospace and Civil Engineering, Harbin Engineering University.
2018/02-2018/03, Humboldt Research Fellow, Aerospace Engineering, Politecnico di Torino
2016/08-2018/03, Humbodlt Research Fellow, Mechanical Engineering, TU Darmstadt
2014/12-2016/06, Research Associate, Architecture and Civil Engineering, City University of Hong Kong
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2018/04-至今，哈尔滨工程大学，航天与建筑工程学院，教授
2018/02-2018/03，意大利都灵理工大学，航天与机械工程系，洪堡学者。合作教授：Erasmo Carrera
2016/08-2018/03，德国达姆施塔特工业大学，机械工程学院，洪堡学者。合作教授：Peter Hagedorn
2014/12-2016/06，香港城市大学，建筑与土木工程系，副研究员。合作教授：K.M. Liew

研究方向
气动热弹性力学；结构振动控制；非线性动力学；计算力学

承担项目
1. 国家自然科学基金青年基金，2019.01-2021.12，主持
2. 哈尔滨工程大学中央高校基本科研业务费专项基金，2019.01-2021.12，主持
3. 国家自然科学基金中-德合作项目，2018.01-2020.12，参加

学术交流
1. The 3rd International Conference on Fluid Dynamics and Aerodynamics, October, 25-26, 2018, Berlin, Germany. (Invited to be Organizing Committee Member) (You being an eminent personality with ample experience in these fields, your thoughts, opinions and decisions are of great value and I would like to put forth a proposal to have you as an Organizing Committee Member and we are confident that your contribution will give a splendid touch to the colloquium as the Speakers/delegates from all around the world will look forward to learn from your works)

2. The 14th International Conference on Dynamical Systems Theory and Applications, December, 2017, lodz, Poland; (Invited)

3. The 20th International Conference on Composite Structures, September, 2017, Paris, France;

4. The 4th International Conference on Dynamics, Vibration and Control, August, 2014, Shanghai, China;

5. 中国力学大会，2011年8月，哈尔滨；

6. 第十二届全国气动弹性学术交流会，2011年6月，承德；

7. 第九届全国动力学与控制学术会议，2012年5月，西安；
招生信息
欢迎如下相关专业的青年才俊攻读博士和硕士学位：
力学、机械、土木、物理、数学、飞行器设计、材料等专业



本科生授课课程
《理论力学》，本科生必修课，64学时；

研究生授课课程
《动力学与控制》，研究生学位课，16学时；

实践性教学
教学研究课题
社会兼职
SCI检索期刊International Journal of Aerospace Engineering编委；

AIAA J., Aerosp. Sci. Technol., Compos. Struct., J. Fluid Struct., Acta Mech., J. Vib Control, Int. J. Mech. Sci., Comput. Methods Appl. Mech. Engrg. 等20余国际知名期刊审稿人；


专利成果


出版著作


发表论文
长期从事气动热弹性分析与颤阵控制、结构振动控制以及非线性动力学等方面的研究工作。截至目前，已在J. Sound Vib.、Nonlinear Dynam.、ASME J. Vib. Acoust.等国际知名期刊共发表和录用SCI检索论文36篇（JCR 1区25篇），论文被SCI他引411次（Web of Science），5篇入选ESI高被引论文。引用专家包括美国工程院院士国际著名计算力学专家J.N. Reddy教授，加拿大工程院院士Q. Wang，欧洲科学院院士John T. Katsikadelis教授以及中国工程院院士杜善义院士等。

[1] Z.G. Song, T.Z. Yang, F.M. Li, E. Carrera, P. Hagedorn. A method of panel flutter suppression and elimination for aeroelastic structures in supersonic airflow. ASME Journal of Vibration and Acoustics, 2018, 140: 064501.

[2] Z.G. Song, F.M. Li. Active aeroelastic flutter analysis and vibration control of supersonic composite laminated plate. Composite Structures, 2012, 94: 702–713.

[3] Z.G. Song, F.M. Li. Active aeroelastic flutter analysis and vibration control of supersonic beams using the piezoelectric actuator/sensor pairs. Smart Materials and Structures, 2011, 20(5): 055013.

[4] F.M. Li, Z.G. Song. Flutter and thermal buckling control for composite laminated panels in supersonic flow. Journal of Sound and Vibration, 2013, 332(22): 5678–5695.

[5] Z.G. Song, F.M. Li, E. Carrera, P. Hagedorn. A new method of smart and optimal flutter control for composite laminated panels in supersonic airflow under thermal effects. Journal of Sound and Vibration, 2018, 414 : 218-232

[6] Z.G. Song, F.M. Li. Aeroelastic analysis and active flutter control of nonlinear lattice sandwich beams. Nonlinear Dynamics, 2014, 76(1): 57–68.

[7] Z.G. Song, F.M. Li. Aerothermoelastic analysis and active flutter control of supersonic composite laminated cylindrical shells. Composite Structures, 2013, 106: 653–660.

[8] Z.G. Song, F.M. Li. Aerothermoelastic analysis of nonlinear composite laminated panel with aerodynamic heating in hypersonic flow. Composites Part B: Engineering, 2014, 56: 830–839.

[9] Z.G. Song, F.M. Li. Aerothermoelastic analysis of lattice sandwich composite panels in supersonic airflow. Meccanica, 2016, 51(4): 877–891.

[10] F.M. Li, Z.G. Song, Z.B. Chen,Active vibration control of conical shells using piezoelectric materials. Journal of Vibration and Control, 2012, 18(14): 2234–2256.

[11] Z.G. Song, F.M. Li. Optimal locations of piezoelectric actuators and sensors for supersonic flutter control of composite laminated panels. Journal of Vibration and Control, 2014, 20(14): 2118–2132..

[12] L.W. Zhang, Z.G. Song*, K.M. Liew^*. Computation of aerothermoelastic properties and active flutter control of CNT reinforced functionally graded composite panels in supersonic airflow. Computer Method in Applied Mechanics and Engineering, 2016, 300, 427–441. (ESI高被引论文)

[13] L.W. Zhang, Z.G. Song*, P. Qiao, K.M. Liew^*. Modeling of dynamic responses of CNT-reinforced composite cylindrical shells under impact loads. Computer Method in Applied Mechanics and Engineering, 2017, 313: 889–903. (ESI高被引论文)

[14] Z.G. Song, F.M. Li, W. Zhang. Active flutter and aerothermal postbuckling control for nonlinear composite laminated panels in supersonic airflow. Journal of Intelligent Material Systems and Structures, 2015, 26(7): 840–857.

[15] Z.G. Song, F.M. Li. Vibration and aeroelastic properties of ordered and disordered two-span panels in supersonic airflow. International Journal of Mechanical Sciences, 2014, 81: 65–72.

[16] Z.G. Song, L.W. Zhang, K.M. Dynamic responses of CNT reinforced composite plates subjected to impact loading. Composites Part B: Engineering, 2016, 99: 154–161.

[17] Z.G. Song, L.W. Zhang, K.M. Liew. Aeroelastic analysis of CNT reinforced functionally graded composite panels in supersonic airflow using a higher-order shear deformation theory. Composite Structures, 2016, 141: 79–90.

[18] Z.G. Song, L.W. Zhang, K.M. Liew. Active vibration control of CNT reinforced functionally graded plates based on a higher-order shear deformation theory. International Journal of Mechanical Sciences, 2016, 105: 90–101.

[19] Z.G. Song, L.W. Zhang, K.M. Liew. Vibration analysis of CNT-reinforced functionally graded composite cylindrical shells in thermal environments. International Journal of Mechanical Sciences, 2016, 115: 339-347.

[20] Z.G. Song, L.W. Zhang, K.M. Liew. Active vibration control of CNT-reinforced composite cylindrical shells via piezoelectric patches. Composite Structures, 2016, 158: 92-100.

[21] L.W. Zhang, Z.G. Song*, K.M. Liew. State-space Levy method for vibration analysis of FG-CNT composite plates subjected to in-plane loads based on higher-order shear deformation theory. Composite Structures, 2015, 134: 989–1003.

[22] F.M. Li, Z.G. Song. Aeroelastic flutter analysis for 2D Kirchhoff and Mindlin panels with different boundary conditions in supersonic airflow. Acta Mechanica, 2014, 225: 3339–3351.

[23] F.M. Li, Z.G. Song. Vibration analysis and active control of nearly periodic two-span beams with piezoelectric actuator/sensor pairs. Applied Mathematics and Mechanics-English Edition, 2015, 36(3): 279–292.

[24] Z.G. Song, F.M. Li. Flutter and buckling characteristics and active control of sandwich panels with triangular lattice core in supersonic airflow. Composites Part B: Engineering, 2017, 108: 334–344.

[25] F.M. Li, Z.G. Song. Aeroelastic properties of sandwich beam with pyramidal lattice core considering geometric nonlinearity in the supersonic airflow. Acta Mechanica Solida Sinica, 2015, 28(6): 639–646.

[26] Z.G. Song, F.M. Li. Investigations on the flutter properties of supersonic panels with different boundary conditions. International Journal of Dynamics and Control, 2014, 2: 346–353.

[27] L.W. Zhang, Z.G. Song, K.M. Liew. Nonlinear bending analysis of FG-CNT reinforced composite thick plates resting on Pasternak foundations using the element-free IMLS-Ritz method. Composite Structures, 2015, 128: 165–175.

[28] L.W. Zhang, Z.G. Song, K.M. Liew. Optimal shape control of CNT reinforced functionally graded composite plates using piezoelectric patches. Composites Part B: Engineering, 2016, 85: 140–149.

[29]L.W. Zhang, Z.G. Song*, K.M. Liew^*. Modeling aerothermoelastic properties and active flutter control of nanocomposite cylindrical shells in supersonic airflow under thermal environments. Computer Method in Applied Mechanics and Engineering.

[30] Y.Y. Chai, Z.G. Song*, F.M. Li^*. Active aerothermoelastic flutter suppression of composite laminated panels with time-dependent boundaries. Composite Structures, 2017, 179: 61-76.

[31] Y.Y. Chai, Z.G. Song*, F.M. Li^*. Investigations on the influences of elastic foundations on the aerothermoelastic flutter and thermal buckling properties of lattice sandwich panels in supersonic airflow. Acta Astronautica, 2017, 140: 176-189.

[32] Y.Y. Chai, F.M. Li, Z.G. Song. Nonlinear Vibration Behaviors of Composite Laminated Plates with Time- Dependent Base Excitation and Boundary Conditions. International Journal of Nonlinear Sciences and Numerical Simulation, 2017, 18(2): 145-161.

[33] Y.Y. Chai, F.M. Li, Z.G. Song, Ch. Zhang. Aerothermoelastic flutter analysis and active vibration suppression of nonlinear composite laminated panels with time-dependent boundary conditions in supersonic airflow. Journal of Intelligent Material Systems and Structures, DOI : 10.1177/**X**.

[34] Y.Y. Chai, F.M. Li, Z.G. Song, Ch. Zhang. Analysis on the aeroelastic stability of open cylindrical shells in subsonic airflow using the theoretical and two-way CFD/CSD coupled methods. International Journal of Acoustics and Vibration. (Accepted, SCI源)

[35] T.Z. Yang, Z.G. Song, E. Clerkin, Y.W. Zhang, J.H. Sun, Y.S. Su, L.Q. Chen, P. Hagedorn. A programmable nonlinear acoustic metamaterial. AIP Advances, 2017, 7 : 095323.
荣誉
1. 德国洪堡学者奖学金，德国洪堡基金会，2015年7月；

2. 哈尔滨工业大学第十九届优秀博士学位论文，哈尔滨工业大学学位委员会，2017年9月；

3. 黑龙江省优秀硕士学位论文；2011年11月；

奖励



照片回忆

2015年ACE门前纪念冬明毕业


2017年与天智师兄共游海德堡


2017年在巴黎参加复合材料结构会议与王立峰教授合影


2018年离开达姆前全家与Hagedorn教授合影


2018年春节期间与大师兄王毅泽共游比萨斜塔


2018年离开都灵前全家与Carrera教授合影留念


2017年洪堡年会参观总统府贝尔维尤宫


2017年陪妻子重回故地（卡鲁）




自定义模块2



自定义模块3