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
Other Post:航空航天系副主任
School/Department:力学与航空航天学院
国峰楠,副教授,博士生导师/硕士生导师,现担任航空航天系副主任。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40余篇,制修订相关标准4项,申请(国防)发明专利20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] Investigation of fracture behaviour of a complex interface crack using a modified interaction energy integral method under thermal shock loading, International Journal of Solids and Structures,314, May 2025, 113317 (SCI, TOP期刊).[3] 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).[4] 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).[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] Statistical characteristics of realistic fiber misalignments of unidirectional composites Fitting distributions and scanning length effects.Thin-Walled Structures. 206, Jan 2025,112621(SCI, A类期刊)[7] Investigation of the Stress Intensity Factor in Heterogeneous Materials Based on the Postprocessing Routine of Commercial Finite Element Software.Applied Sciences, May, 2025, 15, 5827.(SCI, JCRQ2)[8] Numerical Analysis of Pulse Decay Characteristics in Solid Rocket Motors for Different Finocyl Grain Configurations.Aerospace, June 2025, 12, 537.(SCI, A类期刊) [9] Fracture analysis of a non-homogeneous coating structure with dual interfaces under thermal shock, Engineering Fracture Mechanics. 2022,(269),108499. (SCI, JCRQ1). [10] 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).[11]Investigation of the transient thermal shock response of an interface crack using the interaction energy integral method,Theoretical and Applied Fracture Mechanics. 2025(139).104972. (SCI, JCRQ1).[12] Thermal fracture analysis of nonhomogeneous plate with interfaces under uniform heat flow, Journal of Thermal Stresses. 2014,(37):771-793. (SCI). [13] 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.[14] Fracture analysis of a nonhomogeneous coating/substrate system with an interface under thermal shock. Acta Mechanica.2014, (9): 225-229. (SCI)[15] Analysis on the Thermal Fracture Mechanic in Packaging Structure. Advances in Heterogeneous Material Mechanics (ICHMM 2011), 2011:969-973. (EI,ISTP) [16] 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) [17] Thermal shock behavior of a functionally graded material p...
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
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