南京航空航天大学k8凯发集团主页平台管理系统 张夏阳-k8凯发集团

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，先后入选国家级“青年人才托举工程”计划、“科技智库青年人才计划”，南航百强团队成员。主要从事新构型直升机设计、旋翼流固耦合力学、智能/evtol飞行器等方向的研究工作。本科（保送）、博士（直博）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”。主持某专项子课题、国家自然科学基金青年/面上项目、工信部民机项目课题、某yytj项目课题、国家重点实验室基金、研究生教学改革等项目，参研国家自然科学基金重点项目、gf173、两机重大专项等项目。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70余篇（sci、ei收录近30篇）,授权/受理发明专利70余项。担任ast、ijms、ijass、partg：jae等sci期刊审稿人和《航空学报》、《振动与冲击》、《航空工程进展》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，获省部级二等奖1项。

学生培养中重视人文素养与专业能力相融合、综合发展，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，曾获校优秀硕士毕业论文指导教师、中国研究生未来飞行器创新大赛一等奖优秀指导教师、金砖国家工业创新大赛优秀指导教师、南航研究生教学创新大赛一等奖等荣誉。

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（直升机方向），设立下述专业：

（一）基础理论类

• 流固耦合力学（cfd/csd建模、仿真及验证）

• 非线性动力学系统理论建模及分析

• 旋转桨叶的强非定常气动、结构动力学行为模拟分析
  

（二）平台、应用类

• 新构型直升机/新概念飞行器/evtol平台设计分析

• 旋翼类飞行器的机动飞行建模、仿真及验证

• 智能（可变体、可变形）旋翼技术、智能直升机技术

（三）技术服务

还可承担旋翼类飞行器（含直升机）方案设计、场景使用分析及可行性论证，低空经济产业决策咨询，evtol飞行器技术咨询等业务

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.

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。