Zhang Xiayang
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个人情况:

张夏阳,副教授,航空学院、直升机动力学全国重点实验室教师,入选中国科协“青年人才托举工程”国家级青年人才项目,南航首批百强团队“新型旋翼气动及噪声控制创新团队”成员。主要从事新构型直升机设计、旋翼流固耦合力学、高性能旋翼设计等方向的研究工作。本科、博士毕业于北京航空航天大学飞行器设计专业,获“北京市优秀毕业生”。主持GF项目课题、国家自然科学基金青年基金、工信部民机项目课题、国家重点实验室基金、江苏省自然科学基金等项目,参研国家自然科学基金重点项目/面上项目、GF173、海/陆军预研、两机重大专项等国家级项目20余项。在《AIAA Journal》、《Journal of Fluids and Structures》、《International Journal of Mechanical Sciences》、《Chinese Journal of Aeronautics》、《Aerospace Science and Technology》、AIAA系列会议等国内外知名期刊和学术会议上公开发表论文50余篇,其中以第一作者发表SCI收录文章10篇、EI收录文章15篇,授权/受理发明专利50余项,指导研究生多次在国家级、省部级科创竞赛和科研论文中获奖,获GF科学技术进步二等奖1项。担任AST、IJMS、IJASS、PartG:JAE等SCI期刊审稿人和《航空学报》、《振动与冲击》等中文期刊审稿人。主要讲授《高等直升机空气动力学》、《旋翼空气动力学》、《航空航天概论》等课程。

学生培养中重视人文素养与专业能力相融合、综合发展。

研究方向:机械、飞行器设计(航空宇航科学与技术 “双一流”学科下属)

围绕飞行器设计专业,设立新构型/概念飞行器(直升机)设计、流固耦合力学、智能直升机等研究方向

发表学术论文,出版专著情况:

[1] X Y. Zhang, H L. Wang, Q J. Zhao et al., Structural modeling and dynamic analysis of the two-segment deployable beam system. International Journal of Mechanical Sciences (2022), 107633. 

[2] Zhang X Y, Chen X, Zhang K, Zhao Q J, Wang Hualong. Structural modeling and modal analysis of rotor blade during ice accretion. Aerospace Science and Technology, 2022.

[3] Zhang X Y, Zhao Q J, Ma L, Zhang K. Frequency-domain analyses on the aeroelastic characteristics of thrust-vectored system on airship. Aerospace Science and Technology, 2021.

[4] Ma Li, Zhao Qijun, Zhang Kai, Zhang Xiayang, et al. Aeroelastic analysis and structural parametric design of composite rotor blade[J]. Chinese Journal of Aeronautics, 2020.

[5] Zhang Kai, Zhao Qijun, Zhang Xiayang, et al. Analysis of rotor aerodynamic response during ramp collective pitch increase by CFD method[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020. 

[6] Zhang Xiayang, Zhao Qijun, Zhao Guoqing, Wang Bo. Structural characteristics of a propulsion mechanical system considering aeromechanical excitations, International Journal of Mechanical Sciences. 2020, 168: 105227.

[7] Zhang Xiayang, Zhao Meijuan, Liang Haoquan, Zhu Ming. Structural and aeroelastic analyses of a wing with tip rotor[J]. Journal of Fluids and Structures, 2019, 86: 44-69.

[8] Zhang Xiayang, Zhou Xu, Wang Bo,Zhao Qijun, Zhao Guoqing. Dynamic Characteristics of Tilt-Rotor Systems on Advanced High-Altitude VTOL Vehicle[C], ARF 2019:8th Asian and Australian Rotorcraft Forum.

[9] Zhang Kai, Zhao Qijun, Xu Guohua, Zhang Xiayang. Analysis of rotor aerodynamic response during ramp collective pitch increase by CFD method[C], ARF 2019:8th Asian and Australian Rotorcraft Forum.

[10] Zhao Guoqing, Zhao Qijun, Wang Bo, Zhang Xiayang. Effects of Trailing Edge Flap on Rotor Moment Characteristics[C], ARF 2019:8th Asian and Australian Rotorcraft Forum.

[11] Zhang Xiayang, Zhao Meijuan, Liang Haoquan, Zhu Ming. Mode analysis of the thrust-vectored system on an airship[J]. AIAA Journal, 2019, 25(3): 593-611.

[12] Zhang Xiayang, Zhao Meijuan, Liang Haoquan. Improved algorithms applying the numerical Laplace method for response analyses of Timoshenko beam subjected to typical external loads[J]. International Journal of Mechanical Sciences, 2018, 144: 186-204.

[13] Zhang Xiayang, Liang Haoquan, Zhao Meijuan. Fundamental solution and its validation by numerical inverse Laplace transformation and FEM for a damped Timoshenko beam subjected to impact and moving loads[J]. Journal of Vibration and Control, 2019, 25(3): 593-611.

[14] Zhang Xiayang, Zhu Ming, Zhao Meijuan, Wu Zhe. Frequency analysis of wing-rotor system considering flexibility in capsule based on high-accurate method[J]. International Journal of Aeronautical and Space Sciences, 2018, 19(2): 375-387.

[15] Zhang Xiayang, Zhu Ming, Wu Zhe, Zhao Meijuan. Dynamic Analysis of Timoshenko Beam with Arbitrary Constraints and a Further Optimization Based on Least Energy Principle[J]. Mathematical Problems in Engineering, 2018, 2018: 1-19.

[16] Zhang Xiayang, Zhu Ming, Liang Haoquan. Dynamic analysis of the continuous fluid-structure system based on Timoshenko model and considering damping[C]. 58th AIAA /ASCE /AHS /ASC Structures, Structural Dynamics, and Materials Conference. Grapevine, Texas: American Institute of Aeronautics and Astronautics, 2017.

[17] Zhang Xiayang, Liang Haoquan, Guo Xiao, Zhu Ming. Several Concerns of Advanced Airships for Thrust-vectoring Application on Dynamic Study[C]. 23rd AIAA Lighter-Than-Air Systems Technology Conference. Denver, Colorado: American Institute of Aeronautics and Astronautics, 2017.

[18] 张夏阳, 祝明, 武哲. 基于K-V阻尼模型的铁木辛柯梁振动响应分析[J]. 北京航空航天大学学报, 2018, 44(3): 500--507.

  • Educational Experience
  • Work Experience
2006-9 | 2009-7
  • 山西大学附属中学
  • 普通高中毕业

2013-9 | 2019-1
  • 北京航空航天大学
  • 飞行器设计
  • With Certificate of Graduation for Doctorate Study
  • Doctoral Degree in Engineering

2009-9 | 2013-7
  • 北京航空航天大学
  • 飞行器设计与工程
  • University graduated
  • Bachelor's Degree in Engineering

  • Social Affiliations
  • Research Focus
  • 中国力学学会会员

  • 中国航空学会会员

Personal Information

Associate Professor
Supervisor of Master's Candidates

Main positions:航空学会会员

Gender:Male

Alma Mater:北京航空航天大学

Education Level:北京航空航天大学

Degree:Doctoral Degree in Engineering

School/Department:航空学院

Discipline:直升机工程. 机械工程. Flight Vehicle Design

Business Address:明故宫校区

Contact Information:邮箱:zhangxiayang@nuaa.edu.cn

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Research Group

    智能直升机团队

    围绕直升机平台智能技术、智能控制技术、模拟器技术开展研究,融合南航多个“双一流”学科进行团队建设,团队现有教师20余人,研究生50余人。

    倾转旋翼机团队

    已自主研制多款倾转旋翼机,现有教师队伍20余人,专职科研人员15人,研究生队伍30余人

    直升机设计团队

    主要瞄准新构型直升机(旋翼类飞行器)设计和平台技术,瞄准未来10-30年应用需求,团队现有教师队伍15人,博士/硕士研究生40余人。

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