Gender:Male
E-Mail:guofn@dlut.edu.cn
Business Address:综合实验1号楼412B
Contact Information:QQ:280552600
Discipline:Aerospace Propulsion Theory and Engineering. Manufacturing Engineering of Aerospace Vehicle. Flight Vehicle Design

国峰楠

Associate Professor

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Degree:Doctoral Degree
Alma Mater:哈尔滨工业大学
Professional Title:Associate Professor
School/Department:力学与航空航天学院

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国峰楠,博士,副教授,国家二级创新工程师,国际Matriz协会二级认证。毕业于哈尔滨工业大学,曾在航天系统工作多年,参与多项国家重点型号的研发与设计工作,主持/参与多项中央部委课题,主持国家自然科学基金面上项目。入选企业创新型拔尖后备人才,获得大连市高层次人才青年才俊称号,发表论文20余篇,制修订相关标准4项,申请(国防)发明专利10余项。担任International Journal of Fracture, Journal of Applied and Computational Mechanics等多个国际国内期刊的审稿人。曾获得大连理工大学青年教师讲课竞赛一等奖,“课程思政”教学竞赛二等奖,指导学生多次在中国TRIZ杯大学生创新方法大赛、“攀登杯”创新创业竞赛中获奖。目前研究方向主要包括非均匀复合材料热断裂行为研究、先进航天器动力系统设计、热/流/固耦合分析方法研究、航天器结构完整性及寿命评估、固体火箭发动机不稳定燃烧等。欢迎航空宇航科学与技术、材料、力学、机械及数学等专业同学加入,这里有航天推进及材料领域多项前沿课题可以开阔视野、培养能力,并与企业需求无缝对接。在读期间将每月发放科研补助,毕业后将积极帮助推荐到研究院所/企业工作。 欢迎相关领域本科生、研究生加入,在航空航天领域共谋美好未来。1. 学术论文及国防报告 [1] An interaction energy integral method for an interface crack in nonhomogeneous materials containing complex interfaces under thermal loading. International Journal of Solids and Structures.264 (2023) 112089 (SCI, TOP期刊). [2] 可燃芯模材料对环形槽药柱结构完整性影响分析. 固体火箭技术,2023,46(05):747-754. [3] Fracture analysis of a non-homogeneous coating structure with dual interfaces under thermal shock, Engineering Fracture Mechanics. 2022,(269),108499. (SCI, JCRQ1). [4] Investigation of the fracture problem of functionally graded materials with an inclined crack under strong transient thermal loading, Theoretical and Applied Fracture Mechanics. 2022(119).103324. (SCI, JCRQ1).[5] An interaction energy integral method for T-stress evaluation in nonhomogeneous materials under thermal loading,Mechanics of Materials. 2015, (83):30-39. (SCI, JCRQ1). [6] Thermal fracture analysis of nonhomogeneous piezoelectric materials using an interaction energy integral method, International Journal of Solids and Structures. 2014, 51(3): 910-921. (SCI,TOP期刊). [7] Thermal fracture analysis of nonhomogeneous plate with interfaces under uniform heat flow, Journal of Thermal Stresses. 2014,(37):771-793. (SCI).[8] An interaction energy integral method for nonhomogeneous materials with interfaces under thermal loading, International Journal of Solids and Structures, 2012,(49): 355-365. (SCI,TOP期刊). [9] Fracture analysis of a nonhomogeneous coating/substrate system with an interface under thermal shock. Acta Mechanica.2014, (9): 225-229. (SCI)[10] Analysis on the Thermal Fracture Mechanic in Packaging Structure. Advances in Heterogeneous Material Mechanics (ICHMM 2011), 2011:969-973. (EI,ISTP) [11] An interaction energy integral method for an interface crack in two nonhomogeneous plates under thermal loading, Applied Mechanics and Materials. 2013,(275-277):160-163. (EI, ISTP) [12] Thermal shock behavior of a functionally graded material plate with a crack. Applied Mechanics and Materials. 2013,(275-277):152-155. (EI, ISTP) [13] Influences of the continuity of material properties on stress intensity factors of an edge crack. Journal of Harbin Institute of Technology. 2011,(43):16-20. (EI) [14] 功能梯度材料冲击裂纹问题分析.东北大学学报, 2013,(34):108-111. (EI)[15] 推进剂粒子阻尼计算方法及试验研究.第六届空天动力联合会议,2022,成都.[16] 一种复合材料发动机连接设计及仿真分析. 第21届全国复合材料大会(NCCM-21), 2020,呼和浩特.[17] 压力指数动态变化对高压强发动机内弹道的影响研究.中国航天第三专业信息网第四十届技术交流会暨第四届空天动力联合会议,2019,昆明.[18] 固体火箭发动机药柱变形对内弹道的影响研究.固体推进技术,2017(1) 13-16.[19] 求解固体火箭发动机中界面裂纹参数的扩展有限元方法.中国宇航学会第33届学术年会.2016,丹东. [20] 含复杂界面非均匀材料的热断裂力学研究,第16届全国疲劳与断裂学术会议.2012,厦门.[21] 含复杂界面非均匀材料的热机械断裂力学方法研究,第五届全国固体力学青年学者研讨会.2012,大连.[22] Evaluation of the Thermal Interface Cr...

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Research Focus
  • 非均匀复合材料热断裂行为

    先进固体火箭发动机设计

    固体火箭发动机不稳定燃烧

    固体火箭发动机药柱结构完整性

    热结构烧蚀及流固耦合分析

Research Group