张夏阳

个人信息Personal Information

副教授 硕士生导师

招生学科专业:
航空宇航科学与技术 -- 【招收硕士研究生】 -- 航空学院
机械 -- 【招收硕士研究生】 -- 航空学院

性别:男

毕业院校:北京航空航天大学

学历:北京航空航天大学

学位:工学博士学位

所在单位:航空学院

办公地点:明故宫校区

联系方式:邮箱:zhangxiayang@nuaa.edu.cn

电子邮箱:

扫描关注

论文成果

当前位置: 中文主页 >> 科学研究 >> 论文成果

Structural and aeroelastic analyses of a wing with tip rotor

点击次数:

所属单位:航空学院

发表刊物:J. Fluids Struct.

摘要:Based on parametric studies, this paper studies the structural and aerodynamic properties of a typical wing-rotor system by considering additional coupling effects from the tip rotor. The governing equations are established by virtue of Yamanaka's theory and Hamilton's principle in an Euler–Bernoulli precision. In the derivation process, complex mode theory and the Rayleigh–Ritz approach are employed to obtain the analytical solution and the numerical solution, respectively, and a set of trial functions are generated for the sake of reliability. Two aeroelastic models are generated via steady and unsteady aerodynamic models to investigate the divergence and flutter performance, respectively, where the computational p-k method is adopted because of the gyros matrix. In case studies, the effectiveness of the numerical solution is validated through comparative analysis; thereafter, the aeroelastic solutions are further verified. The results demonstrate that the gyro effect and the thrust effect have significant influences on the fundamental structural and aeroelastic performances, and parametric designs have great potential to postpone aeroelastic instabilities. © 2019 Elsevier Ltd

ISSN号:0889-9746

是否译文:

发表时间:2019-04-01

合写作者:Zhao, Meijuan,Liang, Haoquan,朱明

通讯作者:张夏阳