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Substructure-based flutter analysis for a wing-aileron system with freeplay 会议论文
AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018, 2018-01-08
作者:  Xiangyu, W.;  Zhigang, W.;  Chao, Y.;  Xufei, H.
收藏  |  浏览/下载：7/0  |  提交时间：2019/12/30
Consideration of POD interpolation for aeroelastic design with large global structural variations use structural dynamic reanalysis 会议论文
作者:  Li, Dongfeng;  Chen, Gang;  Da Ronch, A.;  Zhou, Qiang;  Li, Yueming
收藏  |  浏览/下载：15/0  |  提交时间：2019/11/26
Mistuning and Structural Coupling Effects on Flutter of Turbomachinery Blades 会议论文
International Conference on Structural Engineering, Vibration and Aerospace Engineering (SEVAE 2013), Zhuhai, PEOPLES R CHINA, 2014-01-01
作者:  Fu, Zhizhong;  Wang, Yanrong
收藏  |  浏览/下载：2/0  |  提交时间：2020/01/06
Aeroelastic Analysis of High Aspect Ratio Wing in Subsonic Flow 会议论文
2013 10TH INTERNATIONAL BHURBAN CONFERENCE ON APPLIED SCIENCES AND TECHNOLOGY (IBCAST), 2013-01-01
作者:  Ahmad, Kamran;  Wuzhigang;  Rahman, Hammad
收藏  |  浏览/下载：3/0  |  提交时间：2020/01/06
Continuum Aeroelastic Model and Flutter Analysis for a Variable-span Morphing Wing 会议论文
2nd International Conference on Mechatronics and Applied Mechanics (ICMAM2012), Taipei, PEOPLES R CHINA, 2013-01-01
作者:  Huang, Ren;  Qiu, Zhiping;  Wang, Xiaojun
收藏  |  浏览/下载：2/0  |  提交时间：2020/01/06
Flutter analysis of X-HALE UAV-A test bed for aeroelastic results validation 会议论文
3rd International Conference on Biomechanics, Neurorehabilitation, Mechanical Engineering, Manufacturing Systems, Robotics and Aerospace, ICMERA 2012, Bucharest, Romania, 2012-10-26
作者:  Ahmad, Kamran;  Rahman, Hammad
收藏  |  浏览/下载：1/0  |  提交时间：2020/01/06
Aeroelastic modeling and analysis of the wing/engine system of a large aircraft 会议论文
International Conference on Advances in Computational Modeling and Simulation (ACMS), Kunming, PEOPLES R CHINA, 2012-01-01
作者:  Wang, Libo;  Wan, Zhiqiang;  Wu, Qiang;  Yang, Chao
收藏  |  浏览/下载：2/0  |  提交时间：2020/01/06
Aerothermal-aeroelastic two-way coupling method for hypersonic flutter of three-dimensional curved panel 会议论文
53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Honolulu, HI, United states, 2012-04-23
作者:  Li, Guoshu;  Wan, Zhiqiang
收藏  |  浏览/下载：2/0  |  提交时间：2020/01/06
A strong coupled CFD-CSD method on computational aeroelastity (EI CONFERENCE) 会议论文
2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China
Xi R.; Jia H.
收藏  |  浏览/下载：63/0  |  提交时间：2013/03/25
In this paper  a strong coupled CFD-CSD method is developed to simulate the aeroelastic phenomena. The CFD solver is based on the finite-volume algorithm for the Navier-Stokes equations on unstructured grid. The CSD solver solves the aeroelastic governing equations in the modal space. Their coupling is realized by a dual-time method. The spring-based smoothing method is adopted to deform and regenerate the aerodynamic grid. Two test cases are selected to validate the authors' method for static and dynamic aeroelastity .The results of the simulation for the static aeroelastic problems of a missile wing show that the Lift Coefficient and Drag Coefficient are severally 7% and 5% lower than those don't consider the elasticity of the wing. The results for the flutter boundary prediction of the AGARD 445.6 wing have been proved much closer to the experiment than using the DLM. This method can describe the effects of fluid viscosity more exactly for highly nonlinear transonic flight conditions. The calculation has proved reliable in the subsonic regime  but not accurate enough in the supersonic regime. 2011 IEEE.  
Flutter derivatives identification of aeroelastic model of hangzhou bay bridge 会议论文
9th International Conference of Chinese Transportation Professionals, ICCTP 2009: Critical Issues in Transportation System Planning, Development, and Management, Harbin, 2009-08-05
作者:  Xu F.Y.;  Hu X.L.;  Chen A.R.
收藏  |  浏览/下载：2/0  |  提交时间：2019/12/24

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