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My Curriculum Vitae
Prof. Dr. Changguo Wang

Ph.D Supervisor in Engineering Mechanics

Deputy Director of Center for Composite Materials

National Key Laboratory of Science and Technology on Advanced Composites in Special Environments

School of Astronautics

Harbin Institute of Technology

------------------

王长国，1979年11月，辽宁大连人。

教授，博士生导师。

复合材料与结构研究所副所长

哈工大 航天学院

作为项目负责人主持承担国家自然科学基金、高分国家重大科技专项、科工局民用航天预研、国防863等项目。 获得国防技术发明二等奖1项、军队科技进步二等奖3项、教育部技术发明二等奖1项，省高校科技奖一等奖1项，全国百篇优秀博士学位论文提名奖，入选教育部新世纪优秀人才支持计划，国家****青年拔尖人才。

Overview
Changguo Wang is a tenured professor in Center for Composite Materials, National Key Laboratory of Science and Technology on Advanced Composites in Special Environments, School of Astronautics at Harbin Institute of Technology (HIT), China.

Professor Wang was born in Dalian, Liaoning Province, China, in 1979. He received the B.S. degree in Engineering Management from Shenyang Jianzhu University, China in 2002; the M.E. and Ph.D degrees in Engineering Mechanics from Harbin Institute of Technology, China in 2004 and 2007, respectively. Wang was a visiting scholar in Institute of Lightweight Structures, Technische Universit？t München in Munich in 2009.

His current research interests include Mechanics of Flexible Structures, Flexible Composite Materials and Structures, Structural Lightweight and Optimization, Structural Buckling/Wrinkling and Vibration, Delamination of Composite Structures, Membrane Crease, Nanoscale Wrinkling Mechanics.

Professor Wang currently serves as a member of council in Society of Composite of Heilongjiang Province.

He is the senior member of CSTAM and CSFCM, a member of AIAA, IASS, and ShellBuckling.

He is the Editoral board of JACM, Front.Mech.Mater., Material Science: Adv. Compo. Struct. etc..

He has served as an organizing committee member, technical program committee member, or scientific committee member for several international conferences, such as MECHCOMP3, M2D2017, MDCE 2016, MEME2016, MSCE2016, and CAC2014, etc..

He was the keynote/session speakers for several international conferences, such as MME2016, MSCE2016, IAC2014, and TCIS2013, etc..

He is the author of over 80 papers in top academic journals such as JMPS, IJSS, Carbon, Proceedings A, IJES, APL, AIAA J., Nanoscale, IJMS, Compo Struct, Soft matter, TWS, Smart mater struct, APL, etc, with more than 800 SCI citations.

He is a referee for ~30 international journals, such as IJSS, IJMS, NC, Strain, JAE, MAMS, Carbon, NS, AIAA J., IJNME, AMS, etc.

Honors(荣誉和奖励)

2007.09,the second prize of military scientific and technological progress award

总装备部军队科技进步二等奖；

2008.09, 哈工大第十届优秀博士学位论文；

2009.09, the nomination award of top 100 outstanding doctoraldissertations in China

全国百篇优秀博士学位论文提名；

2009.11, 哈工大第三届青年教师教学基本功竞赛一等奖；

2011.01, 航院2010年度何鸿燊奖教金(SHAFT)；

2011.11, the Program for New Century Excellent Talents in University

教育部“新世纪优秀人才支持计划”；

2012.07, 哈工大基础研究杰出人才培育计划III类；

2012.11,the third prize of military scientific and technological progress award

总装备部军队科技进步三等奖；

2012.12, 校优秀专兼职工作者；

2013.09, 哈尔滨工业大学教学新秀奖；

2013.11, the second prize of National Defense Technology Invention Award

国防技术发明二等奖；

2013.12, the outstanding youth talent plan of HIT

哈工大“青年拔尖人才选聘计划”；

2014.10, the second prize of military scientific and technological progress award

总装备部军队科技进步二等奖；

2017.02, 黑龙江省高校科技奖一等奖；

2017.05, 全国创新争先奖牌(团队核心成员）；

2017.12,国防科技创新团队奖（团队核心成员）；

2018.01, 教育部高等学校科学研究优秀成果奖技术发明奖二等奖；

2019，第四批国家“****”青年拔尖人才；

Work(工作经历)
TimeInstitution
2007.11-至今CCMS, School of Astronautics, HIT

哈工大航院复合材料与结构研究所
2007.6-2011.3Post-doctorial Stations, School of Materials, HIT

哈工大材料学院博士后流动站
2009Institute of Lightweight Structures, Technische Universit？t München, Munich, Germany (TUM-LLB)

德国慕尼黑工业大学轻型结构实验室（TUM-LLB）


Education(教育经历)

2004.4-2007.4, Engineering Mechanics, HIT, Ph.D

哈尔滨工业大学,博士

2002.9-2004.4, Engineering Mechanics, HIT, M.E.

哈尔滨工业大学,硕士

1998.9-2002.7, Engineering Management, SJU, B.S.

沈阳建筑大学,本科

Others
学校文化素质教育委员会及创新创业教育委员会召开成立大会

http://today.hit.edu.cn/article/2019/05/17/67258

刘远鹏入选第一届优秀博士研究生预留师资博士后

http://www.miit.gov.cn/n**/n**/n**/c**/content.html

http://hitgs.hit.edu.cn/2019/0103/c3330a220159/pagem.htm?from=singlemessage&isappinstalled=0

哈工大在薄膜褶皱研究领域取得重要成果（工信部报道）

http://www.miit.gov.cn/n**/n**/n**/c**/content.html

我校王长国教授课题组在薄膜褶皱研究领域取得重要成果

http://news.hit.edu.cn/2018/0918/c1510a215134/page.htm

http://today.hit.edu.cn/article/58303

我校复合材料与结构研究所王长国教授与美国布朗大学高华健教授合作研究成果《薄膜/塑性基底的褶皱和棘轮行为：锂电池中固态电解质界面的失稳》（Wrinkling and ratcheting of a thin film on cyclically deforming plastic substrate: mechanical instability of the solid-electrolyte interphase in Li-ion batteries）发表在固体力学领域顶级期刊《Journal of the Mechanics and Physics of Solids》(JMPS,影响因子3.566)上。该论文首次实现了薄膜/塑性基底弹塑性失稳问题的理论建模与求解，揭示了褶皱、棘轮与安定的多模式耦联作用机制。论文第一作者为航天学院2014级博士生刘远鹏，导师为王长国教授，我校为第一完成单位，王长国教授和高华健教授为论文的共同通讯作者。

特种环境复合材料技术创新团队 荣获首届全国创新争先奖牌（团队）

http://www.toutiao.com/i****/

（从全国227个团队推选出10个）

“设立全国创新争先奖，是坚持贯彻习近平总书记科技创新思想、团结带领广大科技工作者推动创新驱动发展、向世界科技强国进军的重要举措，是继国家自然科学奖、国家技术发明奖、国家科学技术进步奖之后国家批准设立的又一重大科技奖项，是国家科技奖励体系的重要组成部分和补充。”

复合材料与结构研究所荣获“全国工人先锋号”称号

http://news.hit.edu.cn/b8/39/c1510a178233/page.htm

航天学院复合材料研究所梯队建设：优秀团队是怎样炼成的

http://news.hit.edu.cn/articles/2014/01-03/**.htm

2013教学新秀奖教师介绍

http://cetl.hit.edu.cn/news/Show.asp?id=4162

【美国航空技术发展动向】第四辑——用“布”做的飞机：X-55A先进复合材料货运飞机

转自 http://blog.renren.com/share/**/**

2011年度校科技茶话会

http://news.hit.edu.cn/articles/2011/12-31/**.htm

2009校和院教学竞赛一等奖的相关信息

http://today.hit.edu.cn/articles/2009/06-01/**.htm

http://wenku.baidu.com/view/7f7228f24693daef5ef73ddf.html

**-热烈祝贺刘远鹏通过博士论文预答辩，王亚飞、郭佳铭通过博士开题答辩。


**-热烈祝贺文章Intrinsic edge warping of graphene nanoribbon boost molecular directional motion: toward the novel nanodevices（王亚飞）被PLA录用
https://authors.elsevier.com/tracking/article/details.do?aid=25536&jid=PLA&surname=Wang



about Physics Letters A

https://www.journals.elsevier.com/physics-letters-a



**-热烈祝贺刘远鹏入选第一届优秀博士研究生预留师资博士后
http://hitgs.hit.edu.cn/2019/0103/c3330a220159/pagem.htm?from=singlemessage&isappinstalled=0


**-热烈祝贺文章Graphene kirigami as reinforcement and interfacial bonding effect for toughness and strength of silicon-based nanocomposites（王亚飞）被CMS录用
journal website

https://doi.org/10.1016/j.commatsci.2018.12.034

ABSTRACT:This paper studies the toughness, strength and interfacial bonding effect of graphene kirigami silicon-based nanocomposite (GKSN) using molecular dynamics (MD) simulation. The GKSN model is proposed based on a hybrid potential. It is found that the toughness and maximum strength of GKSN are related to the number of interior cuts and density of kirigami patterns for graphene kirigami. Mechanical response of GKSN has four typical stages, including initial wrinkling, linear increasing, ratcheting and failure. Locking effect can significantly enhance the toughness and maximum strength of GKSN with some rare expectations. With increasing interfacial bonding strength of GKSN, toughness and maximum strength increase steadily. Finally, two novel nanocomposites based on graphene kirigami can be designed. The obtained results in this paper can provide a fundamental understanding of the maximum strength and an insight for enhancing the toughness of graphene kirigami nanocomposite. The proposed mechanisms may have general significances for the design of the next generation “super-tough” and “super-strong” nanocomposites.


**-热烈祝贺文章Dimensional variation of reconfigurable serpentine graphene nanoribbon under tension（王亚飞）被JAP录用
journal website

https://doi.org/10.1063/1.**

ABSTRACT: In this paper, we resort to single-layer graphene nanoribbon (GN) and atomistic simulation to explore the dimensional variation of serpentine graphene. A tensile model of serpentine GN is established, and its topology responses are investigated with some counterintuitive expectations. A laser scanning experiment on the serpentine sheet of paper is performed and compared, which can indirectly reflect the reduced-dimensionality tendency of serpentine GN in tension. As a result, serpentine GN provides a dynamic route of transforming lateral and longitudinal dimensions. Our obtained results can be used to the thermal, electric, or magnetic controlling in future applications.


**-热烈祝贺在2017级硕士开题答辩中，向书毅综合考评成绩排名第一，获一等奖学金；王珂获二等奖学金。



**-热烈祝贺文章Cavitation in inhomogeneous soft solids（康敬天）在Soft Matter发表
journal website

http://pubs.rsc.org/en/content/articlelanding/2018/sm/c8sm01464g/unauth#!divAbstract

http://dx.doi.org/10.1039/C8SM01464G

ABSTRACT: A tiny spherical cavity expands in a homogenous neo-Hookean solid when subjected to an externally applied hydrostatic tension. If the applied tension reaches 2.5 times of the shear modulus of the solid, the cavity expands unboundedly. Such phenomenon is usually referred as cavitation in soft solids. In the previous studies, the soft solid is often assumed to have homogeneous mechanical properties. In this article, we study cavity expansion in inhomogeneous soft solids through analytical formulation and finite element simulation. We find that cavitation in an inhomogeneous soft solid can be greatly different from that in homogenous one. In particular, we show that the relationship between the applied hydrostatic tension and the cavity size can be either monotonic or non-monotonic, depending on the geometry and material properties of the soft solid. We hope the results obtained in this article will be helpful to understand cavitation phenomenon in complex soft materials.


**-热烈祝贺文章“Wrinkling and ratcheting of a thin film on cyclically deforming plastic substrate~（刘远鹏）”在JMPS发表
Wrinkling and ratcheting of a thin film on cyclically deforming plastic substrate: mechanical instability of the solid-electrolyte interphase in Li-ion batterieshttps://doi.org/10.1016/j.jmps.2018.08.006AbstractLithium-ion batteries (LIBs) in consumer electronics, electric cars and large-scale energy storage systems are often susceptible to capacity fading due to mechanical degradation of the solid-electrolyte interphase (SEI) layer on the electrodes. Here we present an analytical model to describe SEI wrinkling and ratcheting behaviors during cyclic lithiation and delithiation of LIBs. The SEI-electrode system is modeled as a bilayer structure consisting of a thin film resting on a plastic substrate. Surface instability is found in such a system under cyclic plastic deformation induced by lithiation and delithiation. A linear perturbation analysis is performed to determine the critical wrinkling strain and wavenumber. The interfacial shear traction induced by surface wrinkling can further lead to plastic ratcheting, and the wrinkling amplitude increases with each lithiation/delithiation cycle. A phase diagram is plotted to characterize and predict different system behaviors, e.g., elastic, elastic wrinkling, shakedown without wrinkling, shakedown with wrinkling, and ratcheting. A series of finite element simulations are performed to validate the theoretical predictions. The analysis suggests that the mechanical instabilities of the SEI, including wrinkling and ratcheting, can be prevented by several strategies, such as introducing an artificial SEI with a sufficiently large stiffness and thickness, and/or with a tensile pre-stress in the SEI.


**-热烈祝贺文章Buckling analysis of an inflated arch including wrinkling based on Pseudo Curved Beam model（薛智明）在TWS发表
journal website

https://www.elsevier.com/journals/thin-walled-structures/0263-8231#description

https://doi.org/10.1016/j.tws.2018.06.044



**-热烈祝贺张则依，尹悦，张佳伟，获得哈工大2018届优秀毕业生称号！
ps：2018届，我的本硕全部学生都获得了优秀毕业生称号，真的很好！


**-热烈祝贺文章Rigid-flexible contatc analysis of an inflated membrane balloon with various contatc conditions（刘猛雄）被IJSS录用并在线发表
scope of IJSS: https://www.journals.elsevier.com/international-journal-of-solids-and-structures/

Paper is published on line.

https://doi.org/10.1016/j.ijsolstr.2018.05.004

ABSTRACT: Considering the Mooney–Rivlin hyperelastic model, a semi-analytical approach is introduced to analyze the rigid–flexible contact behaviors of an inflated membrane balloon between two plates with various interface conditions. This approach is based on the differential formulation and the coupling property of equilibrium equations are well-solved. In order to verify the reliability of the proposed theoretical model, an experimental test is designed, by which some important contact characteristics and patterns (no-slip condition) are obtained. Two special phenomena are observed for the meridian stretch ratio with different friction coefficients. One is that the intersection points of all curves fall in a small interval and the intersection of any two curves represents the same changing rate of the horizontal ordinate, resulting in the maximum difference. The other is the dividing point, where the stretch ratio decreases on the left of it and increases on the right due to the introduction of friction. Under the same contact angle, the larger displacement load should be applied to the balloon for the small friction coefficient condition, resulting in the smaller contact area and internal pressure. In addition, the vulnerable position, direction and contact condition of the balloon are found during the contact process, which happen in the center along the circumferential direction under no-slip condition. These results provide solid guidance and support for our understanding of the rigid-flexible contact behaviors of an inflated membrane balloon.

**-热烈祝贺文章“Elastoplastic folding behavior of membrane ribbon based on plane strain beam theory”（夏振猛）在IJSS发表
https://doi.org/10.1016/j.ijsolstr.2018.03.004

https://www.sciencedirect.com/science/article/pii/S**0969

This paper studies the folding mechanical behaviors of Z-fold membrane ribbon. An elastoplastic folding model is proposed based on the plane strain beam theory, in which a power-law hardening material relation is considered. The folding mechanical characteristics, such as folding force, folding space and shape, are obtained by using the proposed model. The folding experiments and simulations are conducted and the results from experiments and simulations are compared to verify the proposed model. The results in this paper are helpful for the deep understanding of the elastoplastic folding behavior, and the obtained critical folding force or space can be used to guide the crease-free design during the folding.




**-热烈祝贺文章“Growth from buckling to buckling-driven delamination in a film/substrate system with finite thickness”（刘远鹏）在Comp Struct在线发表
journal scope

https://www.journals.elsevier.com/composite-structures/

abstract
Compressing a stiff film bonded to a compliant substrate with finite thickness can lead to various instabilities, including global buckling, local wrinkling, delamination or their concomitant buckling. This paper proposed an analytical model, which integrates global and local interactive effects due to the finite thickness, to reveal the growth from buckling to buckling-driven delamination. The resulting governing non-linear equations (non-autonomous fourth-order ordinary differential nonlinear equations with integral conditions) are then solved by introducing a continuation algorithm, which offers considerable advantages to detect multiple bifurcations and trace a complex post-buckling path. The critical conditions for global buckling, local wrinkling and buckling-driven delamination are carefully studied. Two different growth processes from destabilization to restabilization (snap-back) are captured in the post-buckling range. Moreover,

it is found that the interface toughness and the pre-existing delamination crack length dominates the critical strain for the onset of buckling-driven delamination, and further decide the initial instability mode. Finally, two phase diagrams are plotted to predict both initial and advanced instability modes in such a bilayer system. The phase diagrams can be used to guide the design of film/substrate systems to achieve desired modes of instabilities.

avaliable online

http://www.sciencedirect.com/science/article/pii/S**2179

**-热烈祝贺文章“Bending wrinkling and kink behaviors of inflated beam under local uniform loadings”（刘猛雄）在IJMS发表
http://www.sciencedirect.com/science/article/pii/S**9195
International Journal of Mechanical Sciences

SCOPES

http://www.journals.elsevier.com/international-journal-of-mechanical-sciences/

Abstract

In this paper, analysis of the wrinkling and kink characteristics of the inflated beam under local uniform loadings is presented. Firstly the thin-walled beam modal, which is filled with uniform internal pressure, is established. Next the local uniform loads are applied on the beam. This introduces the load geometric parameters to the equations to predict the wrinkling characteristics. Then the kink, which is similar to a plastic hinge, is assumed to describe the invalid state of the inflated beam for the first time. In order to verify the assumptions of the kink and the theoretical predictions of the wrinkling and kink characteristics, the non-contact experimental tests are performed. Moreover, the theoretical and experimental results, which include the initial wrinkling and kink positions, the critical wrinkling and kink loads, the wrinkling strain, the length of the wrinkled region and the kink angle, are compared. The differences according to these comparisons are less than 10%, which means that the predicted results are reliable. In addition, the local uniform load position and its length as well as the edge shape and the middle cylinder

length of the inflated beam can make great effects on the wrinkling and kink characteristics. These obtained results provide a new insight into the wrinkling and kink behaviors of the inflated beam and give good guidance for designing the inflated structures.


**-热烈祝贺文章“Buckling induced delamination and microflow analysis of film/substrate system”（康敬天）在Composite Structures发表
journal scopes

http://www.journals.elsevier.com/composite-structures/

published online

http://dx.doi.org/10.1016/j.compstruct.2016.11.045

http://www.sciencedirect.com/science/article/pii/S**1552

Abstract

When subjected to uniformly compression, the film/substrate system will present buckling instability. With an appropriate size of pre-exiting interfacial imperfection, there will be local buckling delamination which will result in a buckling delamination induced microchannel. This microchannel has exhibited a potential application of directing and manipulating fluid flow. In this paper, we explore the on-off, evolution and failure process of the buckling delamination induced microchannel with both analytical and finite element method and investigate the flow behavior within this microchannel. We present the analytical solution to determine the critical strain for different film/substrate systems. The linear buckling analysis has been utilized to predict the buckling modes. The characteristics and configuration of the induced microchannel for different compressive strain have been investigated using nonlinear buckling analysis. The Lattice Boltzmann method has been used to study the microflow behavior within the microchannel. The theoretical and numerical buckling delamination analysis, together with the microflow analysis within the microchannel, will lay a foundation to design a flexible microvalve to regulate fluid flow where the use of traditional rigid microvalve is improper in flexible microfluidic device.


**-热烈祝贺 刘远鹏，康敬天，刘猛雄，三人获得研究生国家奖学金！



**-热烈祝贺文章“Global and local interactive buckling behavior of a stiff film/compliant substrate system”（刘远鹏）在 IJSS在线发表
IJSS SCOPES

http://www.journals.elsevier.com/international-journal-of-solids-and-structures/

http://www.sciencedirect.com/science/article/pii/S**2979

ABSTRACT

This paper elucidates the global and local interactive buckling behavior of a stiff film resting on a compliant substrate under uniaxial compression. The resulting governing non-linear equations (non-autonomous fourth-order ordinary differential nonlinear equations with integral conditions) are then solved by introducing a continuation algorithm, which offers considerable advantages to detect multiple bifurcations and trace a complex post-buckling path. The critical conditions for local and global buckling and respective post-buckling equilibrium paths are carefully studied. Two different evolution mechanisms of buckling modes and processes from destabilization to restabilization (snap-back) are observed beyond the onset of the primary sinusoidal wrinkling mode in the post-buckling range. In addition, the shear modulus of an orthotropic substrate acts as a dominant role in the bifurcation portrait. Our results offer better understanding of the global and local buckling behaviors of such a bilayer system, and can open up new opportunities for the design and applications of novel nanoelectronics.




**-热烈祝贺文章“Buckling Delamination Induced Microchannel: Flow Regulation in Microfluidic Devices”在APL出版（康敬天）
APL

SCOPES

http://scitation.aip.org/content/aip/journal/apl/info/about

Buckling Delamination Induced Microchannel: Flow Regulation in Microfluidic Devices

The buckling delamination induced microchannel is employed to regulate fluid flow as a microvalve which can be utilized in microfluidic device. This microvalve consists of a soft substrate and a stiff thin film, between which there is a pre-set small imperfection. Two critical strain values, namely on-off strain and failure strain, have been proposed to determine the working strain interval using analytical predictions. Within this interval, the cross-sectional area of the microchannel can be controlled and predicted by different compressive strain of the film/substrate system. The fluid flow rate within this microchannel can be then estimated by both analytical and numerical simulations and adjusted to satisfy different value by alternating the compressive strain. In addition, a demonstrative experiment has been taken to verified the feasibility of this approach. This flexible microvalve has potential in the application where the use of traditional rigid microvalve is improper in flexible microfluidic device. The method and approach of this paper can provide a general guide for flow rate control in microfluidic devices.



**-热烈祝贺文章"Wrinkling and collapse of mesh reinforced membrane inflated beam under bending"在Acta Astronautica出版(陶强)
Acta Astronautica

http://www.journals.elsevier.com/acta-astronautica/

文章地址如下：

http://www.sciencedirect.com/science/article/pii/S**5112?np=y

abstract

A novel concept of mesh reinforced membrane (MRM) is proposed in this paper. The tensile collapse mechanism of MRM is elucidated based on three obvious deformed stages. An improved Shell-Membrane model is used to predict the wrinkling and collapse of MRM inflated beam which is verified by a non-contact experiment based on the digital image correlation technique. Further the wrinkling details including the wrinkling evolution, pattern, shape, stress distribution are simulated to evaluate the functions of MRM for loading-carrying capacity of inflated beam. Pressure resistant performance of inflated beam was studied at last. The results revealed that MRM shows a great improvement on the collapse moment of inflated beam. MRM contributes to restrain wrinkling evolution by changing the transfer path of loadings which results from dispersing stress distribution and changing wrinkling pattern. The results show good references to the wrinkling control and the improvement of load-carrying capacity of inflated beam.

**-热烈祝贺文章"The interactive bending wrinkling behaviour of inflated beams"在Proceedings A发表(刘远鹏)
Proceedings A全称，Proceedings of the Royal Society of London A: mathematical, physical and engineering sciences.

http://rspa.royalsocietypublishing.org/

文章链接：

http://rspa.royalsocietypublishing.org/content/472/2193/**.abstract

The interactive bending wrinkling behaviour of inflated beams

A model is proposed based on a Fourier series method to analyse the interactive bending wrinkling behaviour of inflated beams. The whole wrinkling evolution is tracked and divided into three stages by identifying the bifurcations of the equilibrium path. The critical wrinkling and failure moments of inflated beam are then able to be predicted. The global-local interactive buckling pattern is elucidated by the proposed theoretical model and also verified by non-contact experimental tests. The effects of geometric parameters, internal pressure and boundary conditions on the buckling of inflated beams are investigated in the end. Results reveal that the interactive buckling characteristics of inflated beam under bending are more sensitive to the dimensions of the structure and boundary conditions. We find that beams which are simply supported at both ends or clamped and simply supported boundary conditions may prevent the wrinkling formation. The results provide significant support for our understanding of the bending-wrinkling behaviour of inflated beams.


**-热烈祝贺薛智明和吉庆祥双双获得优秀硕士学位论文荣誉称号!
祝贺!

继续努力！

希望在博士阶段取得更好的成绩!

**-热烈祝贺文章“An improved molecular structure mechanics method and its application for graphene wrinkling（夏振猛）”在IJES发表
Int. J. Eng. Sci.,3.165

scope

https://www.elsevier.com/journals/international-journal-of-engineering-science/0020-7225#description

文章地址：

http://www.sciencedirect.com/science/article/pii/S**2853


**-热烈欢迎美国RICE大学Boris Yakobson教授来华学术交流与访问。

seminar由王长国教授主持，Boris教授作了题为Predictive theoretical modeling of materials and nanostructures的系列报告，

期间，王长国教授介绍了其在membrane wrinkling方面的研究成果，特别感谢航天学院甄玉宝教授、材料学院徐成彦教授和土木学院的钟晶老师的报告和讨论。

http://today.hit.edu.cn/news/2016/05-26/**RL0.htm



Yakobson教授1982年毕业于俄罗斯科学院，获得物理和应用数学博士学位。1990-1999年到美国北卡罗莱纳州立大学做访问教授，2001年至今任美国莱斯大学Hasselmann基金特聘教授、材料科学与纳米工程教授及化学教授。Yakobson教授长期从事纳米材料理论研究和计算机模拟、低维材料的制备、合成以及性能研究。目前已发表学术论文250余篇，在纳米材料领域具有广泛影响，并获得多项重要奖励，包括Department of Energy Hydrogen Program Award, Nano 50 Innovator Award from Nanotech Briefs (Boston), Royal Society (London) Professorship Award, Department of Energy R & D Award, NASA Faculty Award等。

p.s.:特别感谢清华大学徐志平教授提供的支持。



**-祝贺文章“Post-wrinkling analysis of a torsionally sheared annular thin film by using a compound series method”在IJMS发表（刘远鹏）
International Journal of Mechanical Sciences scope

http://www.journals.elsevier.com/international-journal-of-mechanical-sciences/paper

http://www.sciencedirect.com/science/article/pii/S**0709


**-祝贺文章“Buckling behavior of carbon nanotubes under bending: from ripple to kink”在Carbon发表（刘远鹏）
Carbon scope

http://www.journals.elsevier.com/carbon/



Buckling behavior of carbon nanotubes under bending: from ripple to kink

http://www.sciencedirect.com/science/article/pii/S**1348



**,Iowa State University, Wei Hong（洪伟）教授来访和交流
交流议题和范围：薄膜的褶皱问题；

上午Wei Hong教授参观了实验室，并开展了有关薄膜褶皱问题的交流。



Wei Hong教授的个人主页

http://www.public.iastate.edu/~whong/homepage.html

期待后续的深入广泛的交流和合作。

**-参加IAC2014会议及访问曼尼托巴大学
2014**王长国和夏振猛参加了于加拿大多伦多召开的IAC2014会议，会上作了关于展开结构相关的presentations，会议期间同加拿大约克大学的Jinjun Shan教授进行了深入交谈。会后，前往曼尼托巴大学参观访问了Quan Wang教授的研究室，Nan Wu老师介绍了研究室的研究方向。这是一次愉快和颇多收获的访问，感谢Quan Wang教授和Nan Wu老师的接待和安排。

Quan Wang教授的主页：

http://umanitoba.ca/faculties/engineering/departments/mechanical/staff/profiles/qwang.html



Recent news
2017.03：欢迎博士生王亚飞加入；

2016.9：欢迎张则依硕士加入；

2016.7：薛智明和吉庆祥顺利通过硕士答辩，并双双获得优秀硕士学位论文。张则依顺利通过本科答辩。

2016.4：张则依通过本科中期检查；

2016.2：刘远鹏paper发表于PE;

2016.1：王长国等参加第88次中国力学会青年沙龙；王长国等参与筹备和成立哈工大航天学院与航天一院702所“航天飞行器工程与力学”联合实验室

2016.1：张则依通过本科开题答辩；

2015.10：刘远鹏paper发表于JSV;康敬天paper发表于IJMS;

2015.10：薛智明和吉庆祥顺利通过直博推荐考核；

2015.9：刘远鹏和康敬天以优异成绩顺利通过博士第一学年综合考评；

2015.8：张则依取得保研资格，正式进入课题组；

2015.7：张锦莱和赵字会顺利通过硕士答辩，取得硕士学位；刘猛雄顺利通过本科毕业答辩；夏振猛和陶强顺利通过博士开题答辩；

2015.5：康敬天paper发表于PCCP;

2015.5：王长国等前往国防科大临空所调研和交流；

2014.10：康敬天paper发表于IJMS;夏振猛顺利通过博士第一学年考评；

2014.9：夏振猛paper发表于AIAA J;

2014.7：兰澜获得博士学位；刘远鹏硕士论文获得金奖；

2014.6：兰澜paper发表于AMS;

2014.6：兰澜通过博士学位论文答辩；刘远鹏、康敬天通过硕士学位论文答辩；龚芃通过本科毕业答辩。

2014.5：兰澜和刘远鹏获得优秀毕业生称号；

2014.4：刘远鹏paper发表于Nanoscale;

2014.3：陶强顺利通过博士第一学年考评；刘远鹏和康敬天顺利通过硕士中期检查；龚芃顺利通过本课开题；

2014.2：刘远鹏paper发表于Rsc Adv.;

2013.11：龚芃获得黑龙江省第二届“知识产权杯”高校科技创新竞赛一等奖；

2013.11：刘远鹏获得国家研究生奖学金；

2013.10：兰澜paper发表于Physica E；

2013.7：兰澜、刘远鹏paper发表于RSC Adv.；

2013.7：兰澜paper发表于IJMS；

2013.6：刘远鹏获得研究生特等奖学金；

2013.5：龚芃获得大学生科技创新国家级二等奖；

2013.5：兰澜、刘远鹏paper发表于CMS；

2013.3：刘远鹏paper发表于Nanoscale；

2013.2：兰澜paper发表于IJSS；

2012.12：兰澜paper发表于PCCP；

2012.12：谢军硕士学位论文荣获第八届黑龙江省优秀硕士学位论文；

Research interests(研究方向)

Prof. Wang's major research direction is focused on the membrane materials and structural mechanics of aircrafts. His research interests include Membrane buckling/wrinkling and vibration; Load-carrying ability of inflated membrane structures; Mechanics of flexible composite materials and structures; Mechanics of membrane folding and unfolding; Space rigidization of membrane materials; Structural design theory and its application of space large-scale deployable antenna reflector; Tension-based shape stability of large-scale flexible structures; Light-weighted optimization and fine design of near-space airship structures; Thermal insulation and drag-reducing of envelope material of airship; Structural technology of mixed reinforced super-pressure envelope of light-than-air structures; Non-contact test technologies of static/dynamic perforcement of membrane structures; of Mechanics of graphene pseudo-membrane; Krigami/Origami mechanics of membrane materials and structures;

我所关心的是：柔性复合材料力学、软物质力学和纳米力学中的稳定性问题；

主要研究方向：航天柔性材料与结构、薄膜飞行器结构技术、结构稳定性与控制

学术与科研相关方面（涉及但不局限）：

A 薄膜屈曲/褶皱与振动

B 充气膜的承载失效行为

C 柔性复合材料与结构力学

D 膜结构折叠/展开力学

E 薄膜材料的空间刚化

F 空间展开天线反射器结构设计理论与应用

G 大型柔性结构的张力控型

H 临近空间浮空器结构的轻量化与精细化设计

I 平流层飞艇蒙皮材料隔热与减阻

J 复合增强超压囊体结构技术

K 薄膜结构的非接触静动力性能测试技术

L 石墨烯拟膜结构的力学行为

M 薄膜材料与结构的Kirigami/Origami设计与分析


Projects(科研项目)


作为项目负责人承担过高分国家重大科技专项、国防科工局民用航天预研、国防863、总装武器预研基金、国家自然科学基金、航空科学基金等项目20余项。

2019-2022，弹塑性层合膜结构的屈诱多态失稳力学行为研究，**，国家自然科学基金面上，主持；

2016-2019，柔性网增强充气梁的弯皱耦联行为研究，**，国家自然科学基金面上，主持；

2012-2015，充气膜承力结构整体屈曲与局部皱曲行为研究，**，国家自然科学基金面上，主持；

2010-2012，薄膜褶皱及二次皱曲行为数值分析和模拟研究，**，国家自然科学基金青年，主持；



Courses(讲授课程)

Undergraduate courses

Mechanic sof Deformable Solid (Elastic and Plastic Mechanics) (Autumn course).

Mechanics of Composite Materials (Spring course).

Flexible Materials and Structures (Autumn course).

Graduate courses

Mechanics of Composite Materials and structures (Master)

Advanced Composite Structures (Doctor)

High Temperature Solid Mechnics (Doctor)

复合材料与工程专业本科生课程《柔性复合材料与结构》

复合材料与工程专业本科生课程《变形体力学I》（航天学院重点建设的优秀课程）

复合材料与工程专业、工程力学专业本科生课程《复合材料及其结构力学》（航天学院重点建设的优秀课程）

2010工程力学硕士研究生课程《复合材料结构及其力学》

《先进复合材料与结构》，博士研究生课程

《高温固体力学》，博士研究生课程

Projects(教改项目)

《复合材料专业校内外实习基地建设的研究与实践》. 省科技厅“黑龙江省高等教育教学改革项目”. (JG**). 李金平, 韩杰才, 孟松鹤,张宇民, 王长国. 2012-2014.

《研究生实践教学的研究》. 校“研究生教学改革项目”. 王荣国, 李金平, 孙跃, 王长国, 梁媛媛. 2010-2012.

发表的主要研究论文
The selected papers.
Y.P.Liu, K.Guo, C.G.Wang*, H.J.Gao*. Wrinkling and ratcheting of a thin film on cyclically deforming plastic substrate: mechanical instability of the solid-electrolyte interphase in Li-ion batteries. J. Mech. Phys. Solids. ,2019,123:103-118. https://doi.org/10.1016/j.jmps.2018.08.006

M. X. Liu, C. G. Wang, X. D. Li, Rigid-flexible contact analysis of an inflated balloon with various contact conditions. Int. J. Solids Struct., 2018, 144-145: 218-229.https://doi.org/10.1016/j.ijsolstr.2018.05.004

Z. M. Xia, C. G. Wang, H. F. Tan, Elastoplastic folding behavior of membrane ribbon based on plane strain beam theory. Int. J. Solids Struct., 2018,143:167-174. https://doi.org/10.1016/j.ijsolstr.2018.03.004

C. G. Wang, Y. P. Liu, H. F. Tan, Global and local interactive buckling behavior of a stiff film/compliant substrate system. Int. J. Solids Struct., 2016, 102-103: 176-185. doi: 10.1016/j.ijsolstr.2016.10.006

C. G. Wang, L. Lan, Y. P. Liu, H. F. Tan.Vibration characteristics of wrinkled single-layered graphene sheets. Int. J. Solids Struct., 2013, 50(10):1812-1823.

C. G. Wang, X. W. Du, H. F. Tan, X. D. He, A New Computational Method for Wrinkling Analysis of Gossamer Space Structures, Int. J. Solids Struct., 2009, 46(6):1516-1526.

C. G. Wang, H. F. Tan, X. W. Du and Z. M. Wan. Wrinkling Prediction of Rectangular Shell-Membrane under Transverse In-Plane Displacement. Int. J. Solids Struct., 2007, 44(20): 6507-6516.

Y.P. Liu, C.G. Wang, H. F. Tan. The interactive bending wrinkling behaviour of inflated beams. Proc. R. Soc. A. 2016, 472: **.

C.G.Wang,Y.P.Liu,L.Lan and H.F.Tan.Free transverse vibration of a wrinkled annular thin film by using finite difference method. J. Sound Vib. 2016,363:272-284.

C.G.Wang, J.T.Kang, Z.M.Xue, H.F.Tan, Buckling induced delamination and microflow analysis of film/substrate system. Composite Structures.2017,161:8-14.

Y. P. Liu, C.G.Wang, H .F. Tan. Growth from buckling to buckling-driven delamination in a film/substrate system with finite thickness. Composite Structures. 2017,174:292-300.

C.G.Wang,H.FMode jumping analysis of thin film secondary wrinkling. Int.J.Mech.Sci.2015,104:138-146.

C. G. Wang, L. Lan, H. F. Tan. Secondary Wrinkling Analysis of Rectangular Membrane under Shearing. Int. J. Mech. Sci., 2013,75:299-304.

C. G. Wang, Y. P. Liu, L. Lan, L. Li. H. F. Tan, Post-wrinkling analysis of a torsionally sheared annular thin film by using a compound series method. Int. J. Mech. Sci.,2016,110:22-33.

C.G.Wang, M. X. Liu, H. F. Tan. Bending wrinkling and kink behaviors of inflated beam under local uniform loadings. Int. J. Mech. Sci., 2017,120:136-148.

Q.X.Ji, C.G.Wang, H.F. Tan. Multi-scale wrinkling analysis of the inflated beam. Int. J. Mech. Sci., 2017(126):1-11.

H.F.Tan,J.T.Kang,and C.G.Wang.Study on grooved wall flow under rarefied condition using Lattice Boltzmann Method.Int.J.Mech.Sci.2015,90:1-5.

C. G. Wang, Z. M. Xia, H. F. Tan. An improved molecular structure mechanics method and its application for graphene wrinkling. Int. J. Eng. Sci., 2016, 106:168-178.

C.G.Wang,Y. P. Liu, J. Al-Ghalith, T. Dumitric？, M. K. Wadee, H .F. Tan. Buckling behavior of carbon nanotubes under bending: from ripple to kink, Carbon, 2016,102:224-235.

C. G. Wang, Y. P. Liu. L. Lan, H. F. Tan. Graphene wrinkling: formation, evolution and collapse. Nanoscale, 2013, 5:4454-4461.

C. G. Wang, Y. P. Liu. L. Li, H. F. Tan. Anisotropic thermal conductivity of graphene wrinkles.Nanoscale, 2014, 6:5703-5707.

C. G. Wang, Z. M. Xia, and H. F. Tan.InitialShape Design and Stability Analysis of Rib for Inflatable Deployable Reflector. AIAA J., 2015,53(2):486-492.

J.T.Kang, C.G. Wang, Z.M.Xue, M.X.Liu, H.F.Tan, Buckling Delamination Induced Microchannel: Flow Regulation in Microfluidic Devices. Appl. Phys. Lett., 2016,109:103503.

J.T. Kang, C.G. Wang*, H.F. Tan, Cavitation in inhomogeneous soft solids. Soft Matter, 2018. http://dx.doi.org/10.1039/C8SM01464G.
J.T.Kang, C.G.Wang, S.Q.Cai. Cavitation to Fracture Transition in a Soft Solid. Soft Matter. 2017,13：6372-6376.

C. G. Wang, J. Xie, H. F. Tan.The Modal Analysis and Modal Behavior Investigations on the Wrinkled Membrane Inflated Beam. ACTA Astronaut., 2012,81:660-666.

Q. Tao, C. G. Wang, Z. M. Xue, Z. M. Xie, H. F. Tan. Wrinkling and collapse of mesh reinforced membrane inflated beam under bending. Acta Astronautica. 2016,128: 551-559.

C.G.Wang, J.Xie and H.F.Tan.Vibration Simulations of Wrinkled Membrane Inflated Arch. J. Aerospace Eng. 2014,27(2):414-422.

C. G. Wang, H. F. Tan, X. W. Du. Wrinkling Analysis Method Based on Singular Displacement Component Modification for Membrane Structure. AIAA J. Spacecraft Rockets., 2010,47(1):210-213.

C. G. Wang, X. W. Du and L. M. Zhang. Evaluation of Characteristic and Degree of Wrinkles in Space Membrane Structures. AIAA J. Spacecraft Rockets., 2007,44(1):284-286.

C. G. Wang, X. W. Du and Z. M. Wan. Numerical Simulation of Wrinkles in Space Inflatable Membrane Structures. AIAA J. Spacecraft Rockets., 2006,43(5):1146-1149.

C. G. Wang, X. W. Du and Z. M. Wan. An Experimental Study on Wrinkling Behaviours and Characteristics of Gossamer Space Structures. Strain, 2007,43(4):332-339.

C. G. Wang and H. F .Tan. Experiment and numerical studies on wrinkling control of inflated beam using SMA wires. Smart Mater. Struct., 2010, 19(10):105019(9pages).

C.G.Wang, Y.F.Wang, The mechanical design of a hybrid intellegent hinge with shape memory polymer and spring sheet. Compos. Part.B: Engineering. 2018,134:1-8.

C. G. Wang, L. Lan, H. F. Tan. The physis of wrinkling in graphene membrane under local tension. Phys. Chem. Chem. Phys., 2013, 15(8):2764-2773.

J.T.Kang,C.G.Wang and H.F.Tan.Nanoscale crosslinking in thermoset polymers:A molecular dynamics study. Phys. Chem. Chem. Phys.,2015,17,16519 -16524.

C. G. Wang, Z. Y. Du and H. F. Tan. Initial wrinkling and its evolution of membrane inflated cone in bending. Thin wall. struct., 2012,59:97-102.

Z.M.Xue, C.G.Wang, J.T.Kang, H.F.Tan. Buckling and wrinkling analysis of inflated arch based on Pseudo Curved Beam model. Thin-walled structures. 2018,131: 336-346.

L.Lan,C.G.Wang,and H.F.Tan.Experiment and evaluation of wrinkling strain in a corner tensioned square membrane. Acta Mech.Sinica. 2014,30(3):430-436.

C.G. Wang, M.X. Liu, H.F. Tan. Interactive buckling of inflated envelope under mechanical and thermal loads. Acta Mech. Sinica.. 2016. doi:10.1007/s10409-016-0615-x

C. G. Wang, H. F. Tan and X. D. He. Wrinkle-Crease Interaction Behavior Simulation of A Rectangular Membrane under Shearing. Acta Mech. Sinica., 2011,27(4): 550-558.

C. G. Wang, H. F. Tan and X. W. Du. Pseudo-Beam Method for Compressive Buckling Characteristics Analysis of Space Inflatable Load-Carrying Structures. Acta Mech. Sinica., 2009, 25(5):659-668.

C. G. Wang, H. F. Tan, X. W. Du and X. D. He. A New Model for Wrinkling and Collapse Analysis of Membrane Inflated Beam. Acta Mech. Sinica., 2010,26(4):617-623.

C.G. Wang, M.X. Liu, H.F. Tan. Interactive buckling of an inflated envelope under mechanical and thermal loads. Acta Mech. Sinica., 2017, 33(1): 159-172.

C.G.Wang,J.Xie,H.F.Tan.Vibration evaluation of wrinkled membrance inflated beam.Mech.Adv.Mater.Struc.2015,22(5):376-382.

C. G. Wang, L. N. Mao, X. W. Du, X. D. He. Influence Parameter Analysis and Wrinkling Control of Space Membrane Structures, Mech.Adv. Mater. Struct., 2010, 17(1):49-59.

C. G. Wang, H. F. Tan and X. W. Du. Wrinkling Behaviors of Gossamer Structure with Stretched Annulus-Shape under In-Plane Torsion. Mech.Adv. Mater. Struct., 2008, 15(2):157-164.

C. G. Wang, Z. Y. Du, H. F. Tan. An extremum method for bending-wrinkling predictions of inflated conical cantilever beam. Struct. Eng. Mech., 2013, 46(1): 39-51.

J.T.Kang, H.F.Tan, C.G.Wang, S.Q.Cai. Mechanics modeling of fern cavitation catapult. J. Appl. Phys. 2017,122: 225105.

Y. F. Wang，C. G. Wang, Y . C .Zhang, J .M . Guo, H . F . Tan. Dimensional variation of reconfigurable serpentine graphene nanoribbon under tension. J. Appl. Phys. 2018,125(8),082509.https://doi.org/10.1063/1.**

C. G. Wang, L. Lan, Y. P. Liu, H. F. Tan. Functional group-guided variable frequency characteristics of graphene resonator. RSC Adv., 2013,3(36):16095-16101.

C. G. Wang, Y. P. Liu, L. Li, L. Lan, and H. F. Tan. Abnormal Frequency Characteristics of Wrinkled Graphene. RSC Adv., 2014,4:9395-9400.

C. G. Wang, L. Lan; Y. P. Liu; H. F. Tan, Defect-guided wrinkling in graphene. Comp. Mater. Sci., 2013, 77:250-253.

Xia Z M, Wang C G, Tan H F. Strain-dependent elastic properties of graphene oxide and its composite. Comp. Mater. Sci., 2018, 150C:252-258.

Y. F. Wang , C. G. Wang , Y . C .Zhang, H . F . Tan. Graphene kirigami as reinforcement and interfacial bonding effect for toughness and strength of silicon-based nanocomposites. Comp. Mater. Sci., 2019, 159: 306-315.https://doi.org/10.1016/j.commatsci.2018.12.034

C. G. Wang, L. Lan, Y. P. Liu and H. F. Tan. Multiple component correlation model for elastic modulus of single layer graphene sheets. Physica E. 2014,56:372-376.

Xia Z M, Wang C G, Tan H F. Elastic properties of graphene: A pseudo-beam model with modified internal bending moment and its application. Physica E., 2018, 98C:45-52.
Y. P. Liu, C. G. Wang, L. M. Zhang, H. F. Tan. An evaluation method for nanoscale wrinkle. Physica E. 2016,80:191-194.

C. G. Wang, Y. L. Li, X. W. Du and X. D. He. Simulation Analysis of the Vibration Characteristics of Wrinkled Membrane Space Structure. Int. J. Space Struct., 2007,22(4):239-246.

王长国, 杜星文, 赫晓东. 空间充气薄膜结构的褶皱分析. 力学学报. 2008.(40)3:331-338.

王长国, 杜星文, 万志敏. 空间薄膜结构褶皱的数值模拟最新研究进展. 力学进展. 2007,37(3): 389-397.

杜星文, 王长国, 万志敏. 空间薄膜结构的褶皱研究进展. 力学进展. 2006,36(2):187-199.

王长国, 杜星文, 万志敏. 薄膜褶皱的非线性屈曲有限元分析. 计算力学学报. 2007,24(3):269-274.
C. G. Wang, Y. P. Liu, et al., A Novel Lattice-Based Design and Analysis of Inflatable Wing. 54th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics & Materials Conference, Boston,Massachusetts, 8–11 April 2013. AIAA 2013-1882.

C. C. Wang, et al., A Numerical Algorithm for Eliminating the Singular Stiffness Matrix of Membrane Wrinkling. 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference,Boston, Massachusetts, 8–11 April 2013. AIAA 2013-1930.

C. G. Wang, H. F. Tan and X. D. He. Wrinkle-Crease Interaction Simulation Using Combined MT Model and DP Technique. 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Orlando, Florida, 12–15 April 2010. AIAA 2010-2506.

C. G. Wang, H. F. Tan and X. W. Du. Modified Displacement Component Approach for Wrinkling Analysis of Gossamer Space Structures. 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Sheraton, Waikiki, Hawaii, 23-26 April, AIAA 2007-1822.

C. G. Wang, X. W. Du and Z. M. Wan. Numerical Analysis of Wrinkles in Space Inflatable Membrane Structures. 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Hyatt Regency Newport, Rhode Island, 1-4 May, AIAA 2006-1797.

C. G. Wang, Z. M. Xia, H. F. Tan. Buckling and wrinkling of inflatable support structure of deployable antenna. 65th International Astronautical Congress (IAC2014), Sep.29-Oct.3,2014.

C. G. Wang, Y. P. Liu, H. F. Tan. Torsional wrinkling behaviour of annular thin elastic sheets. 24th International Congress of Theoretical and Applied Mechanics-ICTAM 2016, Montréal, Canada from August 21-26, 2016.

C. G. Wang, Q. Tao, H. F. Tan. Bending capacity of inflated mesh-reinforced-membrane beam. 24th International Congress of Theoretical and Applied Mechanics-ICTAM 2016, Montréal, Canada from August 21-26, 2016.

Authorized invention patents
Patent list

授权发明专利列表


ZL**7.9, 通过修正奇异位移分量消除褶皱计算时刚度矩阵奇异性的方法, 排名第1. 2012

ZL**4.8,薄膜拉剪耦合实验测试装置，排名第1. 2016

ZL**5.1,高精度充气膜结构设计方法，排名第1.2014

ZL**4.3,一种用于控制充气结构构型混编预张力索网的方法，排名第1.2013

ZL**2.X,一种用于超薄柔性膜材拉伸性能测试用的夹具, 排名第1. 2013

ZL**8.6,一种可刚化充气展开径向肋支撑式偏馈抛物面天线，排名第1. 2012

ZL**0.6, 一种带膜径向肋，排名第1. 2016

ZL**7.2,充放气式气囊展卷装置，排名第1.2014

ZL**5.7,一种可微调节间距的径向肋板及调节方法，排名第1.2015

ZL**0.5, 排阵式悬索控型刚柔混合式类翼伞柔性充气机翼无人机，排名第1.2015

ZL**4.8,一种落丝阵式可充气展开机翼，排名第1. 2016

ZL**4.1,保形高空气球，排名第2. 2011

ZL**4.0,充气骨架空中展开式飞艇，排名第2. 2012

ZL**2.9,编织充气薄膜曲面限位网的模具及方法， 排名第2. 2014

ZL**9.6,径向肋充气展开天线的径向肋定位装置，排名第2. 2015

ZL**4.6,一种航天器用充气式径向肋天线尾杆连接件，排名第2. 2014

ZL**0.1,一种径向可展开肋板结构的展开装置，排名第2. 2014

ZL**5.7,一种用于径向肋板展开和收起的装置和方法，排名第2. 2015

ZL**2.3,一种用于制造径向展开肋板结构的模具及方法，排名第2.2015

ZL**6.8,非硬式平流层飞艇自由伸缩装置，排名第2.2015

ZL**1.8, 大口径充气经向肋天线检测装置，排名第2.2016

ZL**5.3,充气环结构多点向心加载试验装置，排名第3. 2014

ZL**2.6,一种基于渐变厚度弹性板的星载抛物面反射天线的抛物面及其成形方法， 排名第3. 2015

ZL**5.3,基于压弯成型的抛物柱面天线反射面及其实现抛物柱面的方法，排名第3.2015

ZL**9.1,一种柔性抛物形天线的增强骨架，排名第3.2015

ZL**5.X,一种带增强骨架的柔性抛物面星载天线，排名第3.2015

ZL**8.7,一种用于高温热合机工作台的表面覆膜吸附固定装置，排名第3.2016

ZL**5.6,一种由形状记忆合金和压电纤维复合材料组合驱动的可变后缘机翼，排名第3. 2015

ZL**9.6,基于MFC的自适应后缘结构的控制装置，排名第3.2015

ZL**9.5,一种折叠充气展开式太阳能电池帆板同步展开机构，排名第4. 2011

ZL**9.8,碳纤维基准尺固定装置, 排名第4. 2012

ZL**.7,一种用于DIC测量的双相机系统的标定板及其标定方法，排名第4.2015

ZL**3.7,一种用于充气卫星的体装式抛物面天线, 排名第4. 2013

ZL**3.0, 一种充气展开抛物柱面天线反射面, 排名第4. 2016

ZL**0.X, 径向肋天线肋板及肋板与中心鼓的连接方法, 排名第4. 2016

ZL**9.6, 充气支撑管与铰链混合支撑展开星载抛物柱面天线, 排名第4. 2016

ZL**5.4，一种可重复使用的变直径充气管密封端头盖，排名第4.2014

ZL**3.5,直管逼近圆环（拱）的掐褶方法，排名第4.2015

ZL**6.X,一种连接充气环用复式搭扣，排名第4.2015

ZL**1.3,一种径向肋天线的肋板尾端与桅杆连接方法，排名第4.2015

ZL**3.X,用于径向肋天线卷曲折叠定位桅杆的装置，排名第4.2015

ZL**8.6,空间充气控制展开支撑臂卷曲折叠模具，排名第4.2015

ZL**0.5,飞艇蒙皮用TPU薄膜减阻微沟槽的热压印制备方法, 排名第4. 2014

ZL**6.0,飞艇蒙皮用具有减阻微沟槽结构的PU或TPU薄膜, 排名第4. 2014

ZL**9.8,飞艇蒙皮用镀AL型TPU薄膜减阻微沟槽的热压印制备方法, 排名第4. 2014

ZL**9.X, 大型空间充气球万向检测底座, 排名第4. 2016

ZL**7.1, 一种径向肋充气展开天线用桅杆, 排名第4. 2016

ZL**3.6, 空间充气展开支撑臂内支撑条打磨装置, 排名第4. 2016

ZL**4.X, 冰窟救生装置, 排名第4. 2016

ZL**6.4,飞艇蒙皮用Al层涂覆型TPU薄膜减阻微沟槽的热压印制备方法, 排名第5. 2014

ZL**9.3,快速可控充气释放机构, 排名第5. 2013

ZL**8.7, 一种充气展开抛物柱面天线的卷曲折叠及充气展开结构, 排名第5. 2016

ZL**1.X,空间站用充气桌，排名第5.2014

ZL**9.9,飞艇蒙皮用镀TiO2型PU或TPU薄膜减阻微沟槽的制备方法, 排名第6. 2014

ZL**6.9,太空飞行器快速充气展开薄膜支撑管, 排名第6. 2014

ZL**5.2,一种双Ω形碳纤维复合材料充气展开臂，排名第6.2014

ZL**7.1,一种测试K型复合材料接头强度的试验夹具，排名第6.2015

ZL**0.4,飞艇蒙皮用TiO2涂覆型PU或TPU薄膜减阻微沟槽的制备方法, 排名第7. 2014

Positions

欢迎喜欢本人研究方向的力学、数学、复合材料和物理等相关专业学生报考本人的研究生。

要求：

具有扎实的数学和相关专业基础，具备良好的英语基础，能够较熟练运用Matlab、ABAQUS/ANSYS/LsDyna/Isight/MS/LAMMPS等结构分析软件；

若具备一定的薄膜结构、复合材料、屈曲与振动、优化、跨尺度模拟与多尺度方法、软物质力学研究经历的学生更佳。

攻读博士的同学，研究生阶段需要有发表SCI/EI文章的经历。

想要攻读本人研究生的同学，请面谈或提供详尽的个人情况介绍。

本人每年招收博士生2名，硕士生1-2名。



my groups



姓名：陶强

出生年月：1989年09月

ID状态：在读博士（2013）

Email：jiujiang_taoqiang@126.com

研究方向：AMS复合材料与结构力学

专业特长：具备纺织材料与复合材料双重专业背景，熟悉纺织材料特性与制备工艺，熟悉复合材料的制备与加工工艺；掌握Ansys和Materials Studio等软件的计算方法。

个人基本情况介绍：

发表文章：

1. Q. Tao, C. G. Wang, Z. M. Xue, Z. M. Xie, H. F. Tan. Wrinkling and collapse of mesh reinforced membrane inflated beam under bending. Acta Astronautica. 2016,128: 551-559.

2. C. G. Wang, Q. Tao, H. F. Tan. Bending capacity of inflated mesh-reinforced-membrane beam. 24th International Congress of Theoretical and Applied Mechanics-ICTAM 2016, Montréal, Canada from August 21-26, 2016.

3. 王长国，陶强. 含缺陷复合材料网格结构的屈曲性能研究。中国力学大会2017，暨庆祝中国力学学会成立60周年大会，北京理工大学，北京。2017.8.14-8.16.
教育背景：

2013.3—至今哈尔滨工业大学 工程力学 博士

2010—2013东华大学 纺织复合材料硕士

2006—2010天津工业大学纺织工程 本科

个人爱好：热爱篮球，NBA勒布朗詹姆斯的忠实球迷；酷爱阅读，喜欢文字，憧憬诗和远方



姓名：刘远鹏

出生年月：1988年

ID状态：在读博士（2012本科毕业于本课题组，保研并于2014年硕士毕业，直博）

Email：liuyuanpeng2009@126.com

研究方向：柔性材料与结构皱曲失稳力学

专业特长：ANSYS, ABAQUS, LAMMPS, MS, ISight等

发表文章：

1. Y.P.Liu, K.Guo, C.G.Wang*, H.J.Gao*. Wrinkling and ratcheting of a thin film on cyclically deforming plastic substrate: mechanical instability of the solid-electrolyte interphase in Li-ion batteries. J. Mech. Phys. Solids.,2018.

2. C. G. Wang, Y. P. Liu, H. F. Tan, Global and local interactive buckling behavior of a stiff film/compliant substrate system. Int. J. Solids Struct., 2016,102-103:176-185.

3. Y.P. Liu, C.G. Wang, H. F. Tan. The interactive bending wrinkling behaviour of inflated beams. Proc. R. Soc. A 2016,472: **.

4. C. G. Wang, Y. P. Liu, L. Lan and H. F. Tan. Free transverse vibration of a wrinkled annular thin film by using finite difference method. J. Sound Vib. 2016,363:272-284.

5. C. G. Wang, Y. P. Liu, J. Al-Ghalith, T. Dumitric？, M. K. Wadee, H .F. Tan. Buckling behavior of carbon nanotubes under bending: from ripple to kink, Carbon. 2016,102:224-235.

6. C. G. Wang,Y. P. Liu, L. Lan, L. Li. H. F. Tan, Post-wrinkling analysis of a torsionally sheared annular thin film by using a compound series method. Int. J. Mech. Sci., 2016,110:22-33.

7. Y. P. Liu, C. G. Wang,L. M. Zhang, H. F. Tan. An evaluation method for nanoscale wrinkle. Physica E. 2016,80:191-194.

8. Y. P. Liu, C.G.Wang, H .F. Tan. Growth from buckling to buckling-driven delamination in a film/substrate system with finite thickness. Composite Structures. 2017,174:292-300.

9. 王长国,刘远鹏,谭惠丰.充气膜承力结构局部与整体相关屈曲行为分析.中国力学大会-2015. 中国上海. 8.15-8.18,2015.

10. C. G. Wang, Y. P. Liu, H. F. Tan. Torsional wrinkling behaviour of annular thin elastic sheets. 24th International Congress of Theoretical and Applied Mechanics-ICTAM 2016, Montréal, Canada from August 21-26, 2016.

发明专利：

1. ZL**0.5, 排阵式悬索控型刚柔混合式类翼伞柔性充气机翼无人机. 王长国, 刘远鹏,龚芃,芦强强,油孝飞,谢超,谭惠丰；申请日2013.5.17. 授权日**.

2. ZL**.X. 一种用于超薄柔性膜材拉伸性能测试用的夹具. 王长国, 张磊, 刘远鹏, 兰澜, 谭惠丰. 申请日2012.06.08. 授权日2013.10.14.

3. ZL**4.3, 一种用于控制充气结构构型混编预张力索网的方法. 王长国，张磊，刘远鹏，兰澜，谭惠丰。申请日2012.6.29.授权日2013.12.03.

4. ZL**7.2, 充放气式气囊展卷装置. 王长国,周涛,刘远鹏,夏振猛,龚芃,谭惠丰；申请日2012.11.22. 授权日2014.02.07.

荣誉：

2013年度研究生国家奖学金

2013年度研究生特等奖学金

个人爱好：篮球、旅游。

目前状态：美国布朗大学访学（高华健院士）



姓名：赵字会

出生年月：1989年08月

ID状态：在读博士（2015年）

Email：zhaozihui89@126.com

研究方向：柔性材料与结构力学

专业特长：ANSYS，ABAQUS，有限元理论；

个人爱好：篮球，听歌，爬山。

目前状态：英国Exeter大学（Prof. Wadde）



姓名: 薛智明

出生年月：1991年6月

ID状态：博士（2016）

Email：**@qq.com

方向：柔性结构稳定性

发表文章：

1. Z.M.Xue, C.G.Wang, J.T.Kang, H.F.Tan. Buckling and wrinkling analysis of inflated arch based on Pseudo Curved Beam model. Thin-walled structures. Accepted in **.

2. Zhiming Xue, C.G.Wang, Huifeng Tan. Buckling analysis of composite mesh reinforced inflated arch. MECHCOMP3. 4-7 July, 2017. Bologna, Italy.

授权与受理发明专利：

1. ZL**6.4. 纵向支撑管与倾斜椭圆环贯通式连接组成的飞艇支撑结构. 王长国，薛智明，谭惠丰，刘远鹏，陶强，吉庆祥. 申请日2015.06.10， 授权日2017.01.04

2. ZL**8.7. 基于S型索网络约束的排环支撑式软式飞艇支撑结构. 王长国, 谭惠丰, 薛志明, 林国昌，卫剑征，刘远鹏. 申请日2015.5.18. 授权日2017.03.08

3. CN**9.0. 基于交叉排布充气环组成的飞艇支撑结构. 王长国，薛智明，谭惠丰，陶强，刘远鹏，康敬天. 申请日2015.09.18

个人基本情况：

2016—至今 哈尔滨工业大学 工程力学 博士

2014—2016哈尔滨工业大学 工程力学 硕士

2010—2014 沈阳化工大学 理论与应用力学 本科

爱好：篮球，台球

姓名：王亚飞

出生年月：1990年10月

ID状态：博士（2017.3申请考核）

Email：woofigo@foxmail.com

方向：柔性材料与力学

发表文章：

C. G. Wang, Y. F. Wang. The mechanical design of a hybrid intelligent hinge with shape memory polymer and spring sheet. Composites Part B: Engineering. 2018,134:1-8.

Y. F. Wang，C. G. Wang, Y . C .Zhang, J .M . Guo, H . F . Tan. Dimensional variation of reconfigurable serpentine graphene nanoribbon under tension. Journal of Applied Physics, 2018,125(8),082509.

Y. F. Wang , C. G. Wang , Y . C .Zhang, H . F . Tan. Graphene kirigami as reinforcement and interfacial bonding effect for toughness and strength of silicon-based nanocomposites. Computational Materials Science, 2019, 159: 306-315.

Y. F. Wang，C. G. Wang, H . F . Tan. Intrinsic edge warping of graphene nanoribbon boost molecular directional motion: Toward the novel nanodevices. Physics Letters A, 2019.

授权与受理发明专利：

1. **2 基于柱状充气囊的可重复柔性航天服关节加劲装置及其使用方法. 王长国，谭惠丰，王亚飞，康敬天

2. **1一种基于形状记忆聚合物的缓释阻尼机构. 王长国，谭惠丰，王亚飞

3. **64一种分体式弱关联模块化浮空平台. 王长国，谭惠丰，王亚飞，邱星翰

4. **83 一种恒升力充气闭孔微结构浮空材料单元.王长国，谭惠丰，王亚飞，邱星翰

个人基本情况介绍：

2017.3—至今哈尔滨工业大学工程力学博士

2014.9—2016.6哈尔滨工业大学 固体力学硕士

2009.9—2013.6东北农业大学机械工程本科

荣誉：

中国研究生未来飞行器创新竞赛二等奖

罗麦科技奖学金

三好学生

综合素质二等奖学金
爱好：

安静
姓名：郭佳铭

出生年月：1993年01月

ID状态：硕博连读（2016硕士 2017博士）

Email：**@qq.com

研究方向：柔性材料与结构力学

个人基本情况介绍：

教育背景：

2016.9-至今哈尔滨工业大学工程力学硕博连读

2011.9-2015.6 东北农业大学 水利工程 本科

个人爱好：旅行、看书、听歌

活动：羽毛球大赛，女子单打一等奖



姓名：张则依

出生年月：1994年06月

ID状态：博士（2018）

Email：**@qq.com

研究方向：软物质力学

发表文章：

1. 张则依，刘远鹏，向书毅，王长国，柔性全固态超级电容器电极的设计与制备，第二届全国新型太阳能电池大会，2016. 中国深圳. 11,2016.

授权与受理发明专利：

1. CN**6.0. 一种利用μ#LED来稳定控温的柔性电子器件. 王长国，张则依，谭惠丰，刘远鹏，向书毅. 申请日2017.09.01

个人基本情况：

2018—至今哈尔滨工业大学工程力学 博士

2016—2018 哈尔滨工业大学工程力学 硕士

2012—2016 哈尔滨工业大学复合材料与工程 本科

荣誉：

国家奖学金（硕士）

校优秀毕业生（本科，硕士）

校优秀共青团员（硕士）

保研（毕业设计（论文）重点支持项目）

法学双学位

省级三好学生

优秀学生干部标兵

校级十佳团支书

爱好：健身，旅行。



姓名：张佳伟

出生年月：1996年06月

ID状态：博士（2018）

Email：**@qq.com

研究方向：薄膜褶皱力学

技能：matlab、abaqus、fenics

个人基本情况：

2018-至今 哈尔滨工业大学 工程力学 博士（直博）

2014-2018哈尔滨工业大学复合材料与工程 本科

荣誉：

哈工大优秀毕业生

大学生创新创业计划二等奖

校优秀毕业生

校三好学生

爱好：散步，看书，美食。



姓名：张季

出生年月：1993年02月

ID状态：博士（2018）

Email：**@qq.com

研究方向：薄膜折叠展开

个人基本情况：

2018-至今 哈尔滨工业大学 工程力学 博士

2015-2018大连理工大学工程力学 硕士

荣誉：

蒋震奖学金

爱好：游泳，乒乓球，羽毛球。



姓名：向书毅

出生年月：1995年08月

ID状态：硕士在读

Email：**@qq.com

研究方向：核壳结构稳定性

专业特长：abaqus, matlab, office, solidworks

发表文章：

Shuyi Xiang, Changguo Wang. Non-sinusoidal buckling patterns turned by micro-structure of film/substrate system[C]. Engineering Mechanics Institute International Conference 2018, 2-4 November, 2018,77.

个人基本情况：

2017—至今哈尔滨工业大学工程力学硕士

2013—2017 哈尔滨工业大学复合材料与工程本科

荣誉：

第六届全国大学生数学竞赛（初赛）全国一等奖

2014—2015校优秀团员标兵

罗麦科技航天奖学金

哈尔滨工业大学一等学业奖学金

参加活动：

2018.04 参加柔性复材党支部羽毛球赛

2018.11 在工程力学国际会议EMI-IC2018作学术汇报

爱好：听歌，旅行。

升学：清华大学固体力学读博



姓名：王珂

出生年月：1993年8月

ID状态：硕士在读

Email：17s118147@stu.hit.edu.cn

研究方向：考虑蠕变膜面失稳行为

个人基本情况：

2017—至今哈尔滨工业大学工程力学硕士

荣誉：

校优秀三好学生

校一等奖学金

国家励志奖学金

校级周培元力学竞赛二等奖

哈工大二等学业奖学金

2018.05“上纬杯”第四届全国大学生复合材料设计与制作大赛优秀奖

2018.11.10-2018.11.11年获黑龙江省首届大学生中式台球锦标赛团体冠军

爱好：台球，乒乓球，网球，篮球，滑冰，唱歌，书法。

升学：哈工大读博（推荐攻博）



姓名：尹悦

出生年月：1996年03月

ID状态：硕士在读

Email：**@qq.com

研究方向：薄膜折痕力学

个人基本情况：

2018—至今哈尔滨工业大学工程力学硕士

2014—2018 哈尔滨工业大学工程力学本科

荣誉：

2016年中国白俄罗斯青少年机器人比赛一等奖

2016年中国国际飞行器设计挑战赛暨科研类全国航空航天模型锦标赛三等奖

2018年第二届维谛杯三等奖

第七届祖光杯创意创新创业大赛银奖

哈工大优秀团干部，优秀学生干部，三好学生

哈工大优秀毕业生

爱好：睡觉，游泳。



姓名：邱星翰

出生年月：1995年06月

ID状态：硕士在读

Email：18S118151@stu.hit.edu.cn

研究方向：待定

技能：ansys、solidworks、abaqus、3D打印

个人基本情况：

2018-至今 哈尔滨工业大学 工程力学硕士

2014-2018长沙理工大学 工程力学 本科

荣誉：

哈工大硕士二等奖学金

爱好：篮球，旅行。

活动：柔性复材党支部羽毛球赛


***************************************************************************

姓名：毛丽娜

ID状态：2009年博士毕业

博士论文：《充气膜结构反射面的形态分析与优化方法研究》

工作单位：航天一院702所



姓名:杜振勇

ID状态：2012年博士毕业

博士论文：《充气梁弯皱特性研究》
Email：duzy59@163.com
工作单位：中电十四所



姓名：兰澜

ID状态：2014年博士毕业；

博士论文：《薄膜褶皱的宏观和微观机理与特性的研究》

Email:lanlan5611@126.com

毕业去向：航天5院504所上海研发中心

姓名：夏振猛

出生年月：1988年05月

ID状态：2018年博士毕业

Email：xiazhenmeng@126.com

研究方向：薄膜结构的折痕力学行为

发表文章：

1. Xia Z M, Wang C G, Tan H F. Elastoplastic folding behavior of membrane ribbon based on plane strain beam theory[J]. International Journal of Solids and Structures, 2018, 143C:167-174.

2. Xia Z M, Wang C G, Tan H F. Strain-dependent elastic properties of graphene oxide and its composite[J]. Computational Material Science, 2018, 150C:252-258.

3. Xia Z M, Wang C G, Tan H F. Elastic properties of graphene: A pseudo-beam model with modified internal bending moment and its application[J]. Physica E: Low-dimensional Systems and Nanostructures, 2018, 98C:45-52.

4. Wang C G, Xia Z M, Tan H F. An improved molecular structure mechanics method and its application for graphene wrinkling[J]. International Journal of Engineering Science, 2016, 106:168-178.

5. Wang C G, Xia Z M, Tan H F. Initial shape design and stability analysis of rib for inflatable deployable reflector[J]. AIAA Journal, 2015, 53(2):486-492.

6. Wang C G, Xia Z M, Tan H F. Buckling and wrinkling of inflatable support structure of deployable antenna[C]. The 65th International Astronautical Congress, Canada, Toronto, 29 September-3 October, 2014.

7.Xia Z M，Wang C G, Tan H F. Effects of graphene mass fraction and aspect ratio on elastic properties of graphene-based composites[C]. The 21st International Conference on Composite Materials, Xi’an, China, 20-25 August, 2017.

教育背景：

2013.9-2018.7哈尔滨工业大学工程力学 博士

2011.9-2013.7哈尔滨工业大学工程力学 硕士

2006.9-2010.7哈尔滨工业大学 数学与应用数学 本科

博士论文:《薄膜结构的弯折与拉展变形行为研究》

毕业去向：哈尔滨工程大学

姓名：康敬天

出生年月：1989年02月

ID状态：2018年博士毕业

Email：kangjingtian@hotmail.com

研究方向：层合结构失稳与分层

专业特长：ABAQUS、有限元理论、C++、Matlab、ProE、Hypermesh

个人基本情况介绍：

发表文章：

1. J.T. Kang, C.G. Wang, H.F. Tan, Cavitation in inhomogeneous soft solids. Soft Matter, 2018.

2. J.T. Kang, C.G. Wang, S.Q. Cai, Cavitation to Fracture Transition in a Soft Solid, Soft Matter[J], 2017, 13(37): 6372-6376.

3. J.T. Kang, K. Li, H.F. Tan, C.G. Wang, S.Q. Cai, Mechanics modelling of fern cavitation catapult[J]. Journal of Applied Physics, 2017, 122: 225105.

4. J.T. Kang, C.G. Wang, Z.M. Xue, H.F. Tan, Buckling delamination induced microchannel: Flow regulation in microfluidic devices[J], Applied Physics Letters , 2016, 109.10: 103503.

5. H.F. Tan, J. T. Kang, and C. G. Wang, Study on grooved wall flow under rarefied condition using the Lattice Boltzmann Method[J], International Journal of Mechanical Sciences, 2015, 90: 1-5.

6. C.G. Wang, J. T. Kang, Z.M. Xue, H.F. Tan, Buckling induced delamination and microflow analysis of film/substrate system[J], Composite Structures, 2017, 161:8-14.

7. J.T. Kang, C.G. Wang, H.F. Tan, Nanoscale crosslinking in thermoset polymers: a molecular dynamics study[J], Physical Chemistry Chemical Physics, 2015, 17(25): 16519-16524.

8. 谭惠丰、康敬天、卫剑征，王长国, 三角形沟槽飞艇蒙皮表面的流场分析, 哈尔滨工业大学学报, 2014,46(7):32-35.

9. 康敬天、王长国、谭惠丰, 薄膜基体层合结构的屈曲分层行为分析,第十九届全国复合材料学术会议，2016.

教育背景：

2014.9-2018.7哈尔滨工业大学工程力学 博士

2012.9-2014.7哈尔滨工业大学工程力学 硕士

个人爱好：乒乓球，篮球，羽毛球。

博士论文：《柔性固体的失稳与断裂行为研究》

毕业去向：东北大学



姓名：谢军

ID状态：2012年7月硕士毕业

硕士论文：《充气膜结构的褶皱及振动特性研究》（黑龙江省优秀硕士学位论文）

工作单位：中国科学院长春光学精密机械与物理研究所

邮箱：xiejun.2010@163.com



姓名：崔宇佳

ID状态：2012年7月硕士毕业

硕士论文：《充气翼三维初始形态分析》

工作单位：空中客车（北京）工程技术中心

email：**@qq.com



姓名：张磊

ID状态：2013年硕士毕业

硕士论文：《柔性膜条增强蒙皮的承力性能研究》

毕业去向：留法Arts et Métiers ParisTech

Email：zh**@hotmail.com

姓名：刘远鹏

ID状态：2014年硕士毕业

硕士论文：《石墨烯褶皱行为及具皱石墨烯的力学性能研究》 （优秀硕士学位论文金牌）

毕业去向：直博



姓名：张锦莱

ID状态：2015年硕士毕业

硕士论文：《薄膜结构的屈曲与振动特性研究》

毕业去向：天津航天机电设备研究所

Email：**@qq.com


姓名：薛智明

ID状态：2016年硕士毕业

硕士论文：《索网络增强充气拱结构的屈曲行为分析》 （优秀硕士学位论文）

毕业去向：直博



姓名：吉庆祥

ID状态：2016年硕士毕业

硕士论文：《软式飞艇囊体结构弯皱特性分析》 （优秀硕士学位论文）

毕业去向：读博

Email：royrommel1@126.com



姓名：刘猛雄

出生年月：1991.07

ID状态：硕士毕业（2015）

Email：**@qq.com

方向：多场耦合条件下柔性结构的屈曲行为

个人基本情况：

2015.9—至今 哈尔滨工业大学工程力学研究生

2011.9—2015.7 哈尔滨工业大学复合材料与工程本科

爱好：篮球，健身，跑步。

发表文章：

1.C.G. Wang, M.X. Liu, H.F. Tan. Interactive buckling of inflated envelope under mechanical and thermal loads. Acta Mech. Sinica. 2017,33(1): 159-172.

2.C.G.Wang, M. X. Liu, H. F.Tan. Bending wrinkling and kink behaviors of inflated beam under local uniform loadings. Int. J. Mech. Sci. .2017,120:136-148.

毕业去向：清华大学读博


姓名：刘远鹏

ID状态：2012年本科毕业

毕业论文：《充气机翼点阵式设计及其承力性能优化分析》

毕业去向：读研

姓名：张锦莱

ID状态：2013年本科毕业

毕业论文：《石墨烯太赫兹高频振动特性的分子动力学模拟》

毕业去向：读研



姓名：龚芃

ID状态：2014年本科毕业

毕业论文：《一种可刚化机翼的结构设计及其承力性能分析》

Email：gongpengcq@163.com

毕业去向：加拿大留学，University of Calgary

研究方向：纳米力学

姓名：刘猛雄

ID状态：2015年本科毕业

毕业论文：《平流层热环境下软式飞艇囊体结构的屈曲分析》

毕业去向：读研

姓名：张则依

ID状态：2016年本科毕业

毕业论文：《薄膜基底层合结构压缩屈曲与u000B分层特性分析》

毕业去向：读研

姓名：向书毅

ID状态：2017年本科毕业

毕业论文：《石墨烯/聚苯胺柔性超级电容器的变形对电容性能的影响分析》

毕业去向：读研

姓名：张佳伟

ID状态：2018年本科毕业

毕业论文：《薄膜结构的褶皱行为分析与幅度反演》

毕业去向：直博

姓名：张则依

ID状态：2018年硕士毕业

毕业论文：《柔性薄膜基底层合结构的屈曲失稳行为研究》

毕业去向：读博

姓名：张藻旭

ID状态：2018年本科在读

研究方向：二维三轴编织材料力学

毕业去向：读研



指导和协助指导的学生
博士研究生(含副导师）
2018级：

张则依，研究方向，薄膜结构稳定性；

张佳伟，研究方向，薄膜结构稳定性；

张季， 研究方向，薄膜结构稳定性；

2017级：

王亚飞，研究方向，柔性材料与结构力学；


郭佳铭，研究方向，柔性材料与结构力学；

2016级（直博）：

薛智明，研究方向，结构的屈曲与分岔；

2015级：

赵字会，研究方向，软物质失稳力学；

2014级：

刘远鹏（直攻博），研究方向：褶皱力学；

康敬天（直攻博，副导师）：多尺度模拟；

2013级：

夏振猛，研究方向：结构的折痕力学行为研究；

陶强，可刚化mesh材料与结构；副导师

2010级：
兰澜(2014毕业)，博士论文：薄膜褶皱的宏观和微观机理与特性的研究. 毕业去向：航天5院(上海)，副导师

2008级：
杜振勇（2012毕业）博士论文：充气梁弯皱行为研究.毕业去向：南京14所，副导师
2006级：
毛丽娜（2010毕业）博士论文：充气膜结构反射面的形态分析与优化方法研究，毕业去向：中国运载火箭技术研究院（航天一院702），副导师



博士研究生（协助指导）

2007级：

王超（2009毕业） 研究方向：飞艇结构设计与分析. 毕业去向:中国空间技术研究院（5院总体，钱学森实验室）



硕士研究生

2018级

尹悦， 研究方向，薄膜折痕力学；

邱星翰，研究方向，待定；

2017级

王珂， 研究方向，考虑蠕变膜面失稳行为；

向书毅，研究方向，核壳结构稳定性；

2016级：

张则依，研究方向，层合薄膜压缩屈曲与分层；


2015级：

刘猛雄，研究方向，多场耦合作用下柔性结构的屈曲行为；

2014级：

薛智明，研究方向，薄膜结构的相关屈曲（优秀硕士学位论文，直攻博）；

吉庆祥，研究方向，飞艇结构的热稳定性（优秀硕士学位论文，直攻博）；

2013级：

张锦莱，研究方向：圆环薄膜结构的屈曲与振动研究；（天津航天机电设备研究所，航天科技5院518）

赵字会，研究方向：泡沫填充可刚化机翼结构的承力性能分析（协助指导）（读博）

2012级：

刘远鹏，研究方向：石墨烯褶皱行为及具皱石墨烯的力学性能研究（研究生特等奖学金，优秀硕士学位论文，金牌）（读博）

康敬天，研究方向：微尺度流动的格子Boltzmann方法及其模拟研究（读博）

2011级：
张磊，研究方向：柔性索网增强蒙皮的承力性能研究（研究生特等奖学金）（工作去向：留学法国国立高等工程技术学院，Arts et métiers ParisTech, ENSAM）

夏振猛（协助指导），研究方向：天线面支撑结构张力特性分析与优化（工作去向：读博）
罗锡林（协助指导），研究方向：CFRP整体式桁架制备与力学性能分析（工作去向：读博）
2010级：
谢军，研究方向：充气膜承力结构屈曲与振动特性 （工作去向：中科院长光所）（研究生特等奖学金，省优秀硕士论文）
杨留义（协助指导），研究方向：飞艇结构设计及其气弹特性分析（船舶725所洛阳双瑞集团）
熊波（协助指导），研究方向：狭长三角桁架结构承载性能分析（攻读博士）
崔宇佳（协助指导），研究方向：充气翼三维初始形态分析（工作去向：空客北京工程技术中心）

2009级：

胡晓蒙（协助指导），硕士论文：Y型和K型复合材料桁架接头承载性能分析，毕业去向：中航科工集团7801研究所

2007级：（2009年毕业）
郭正（协助指导），硕士论文：基于形状记忆合金丝充气薄膜管弯皱变形控制研究，毕业去向：中航通用飞机责任公司
于宁（协助指导），硕士论文：充气环结构的承载能力分析，毕业去向：哈尔滨汽轮机厂有限责任公司
2006级：（2008年毕业）
杜振勇（协助指导），硕士论文：充气管结构的承载能力分析，毕业去向：哈尔滨工业大学读博
鲁明宇（协助指导），硕士论文：基于形状记忆材料的薄膜皱曲形变控制研究，毕业去向：香港理工大学读博



本科生
2011级：

刘远鹏毕业论文（2012毕业）：充气机翼点阵式设计及其承载性能优化分析（保研）

2012级：

张锦莱毕业论文（2013毕业）：石墨烯太赫兹高频振动特性的分子动力学模拟（读研）

2013级：

龚芃，研究方向：一种可刚化机翼的结构设计及其承力性能分析（加拿大，University of Calgary）

2014级：

刘猛雄，研究方向：软式飞艇结构的热屈曲问题（读研）

2015级：

张则依，研究方向：层和柔性结构表面失稳问题（保研）

2016级：

向书毅，研究方向：结构稳定性

2017级：

张佳伟，研究方向：薄膜褶皱力学

2018级：

张藻旭，研究方向：二维三轴编织复合材料力学

本科班级
2008级：（已毕业）

**班（复合材料与工程专业） （校三好班级标兵，校优秀团支部标兵，21人中18人录取研究生，1人出国，2人参加工作，13名党员）



Contact


Prof., Dr., Changguo Wang (王长国)

Tel. No.:+86-**

Fax No.:+86-**



Postcode:150080

Address:

Room no. A416, CCMS, HIT Science

Park, No.2, Yikuang Str., Nangang Dist.

Harbin.



(哈市南岗区一匡街2号, 哈工大科学园A栋416室)

Blog：http://blog.hit.edu.cn/www/