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浏览/检索结果: 共6条，第1-6条 帮助 已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择作者升序作者降序题名升序题名降序发表日期升序发表日期降序提交时间升序提交时间降序 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 Aeroelastic response  Approximate methods  Flutter boundaries  Proper orthogonal decompositions  Reconstruction method  Reduced order models  Structural parameter  Structural variations   Effects of Coverage of Dynamic Mesh Region on Efficiency and Accuracy of Coupled Fluid Structure Simulation for Blade Flutter 期刊论文 Tuijin Jishu/Journal of Propulsion Technology, 2017, 卷号: 38, 页码: 2086-2092 作者:  Wang, Rui;  Zhong, Ji-Ze;  Xu, Zi-Li;  Kan, Xuan-En 收藏  |  浏览/下载：4/0  |  提交时间：2019/11/26 Aeroelastic stability  Blade  Compressor blades  Dynamic mesh  Flutter boundaries  Logarithmic decrement  Maximum displacement  Reynolds Averaged Navier-Stokes Equations   Time-space synchronizing fluid structure coupling method using a fast dynamic mesh technique 期刊论文 Zhendong Gongcheng Xuebao/Journal of Vibration Engineering, 2017, 卷号: 30, 页码: 41-48 作者:  Zhong, Ji-Ze;  Xu, Zi-Li 收藏  |  浏览/下载：4/0  |  提交时间：2019/11/26 Coupling iteration  Dynamic mesh  Fluid structure couplings  Flutter boundaries  Reynolds - Averaged Navier-Stokes  Structural vibrations  Time synchronization  Time-space   An efficient dynamic mesh method based on pseudo elastic solid 期刊论文 Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University, 2016, 卷号: 50, 期号: [db:dc_citation_issue], 页码: 132-138 作者:  Zhong, Jize;  Xu, Zili;  Tao, Lei 收藏  |  浏览/下载：3/0  |  提交时间：2019/12/02 Dynamic mesh method  Elastic solids  Fluid structure coupled vibration  Fluid structure couplings  Flutter boundaries  Modal superposition  Mode superposition  Nodal displacement   Numerical simulation and wind tunnel testing of flutter about an all- Movable horizontal tail at transonic speeds 会议论文 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014, St. Petersburg, Russia, September 7, 2014 - September 12, 2014 作者:  Qian W;  Yang GW(杨国伟);  Zheng GN(郑冠男);  Zhang GJ 收藏  |  浏览/下载：15/0  |  提交时间：2017/05/27 All-movable horizontal tail  Flutter boundaries  Overload factors  Structure dynamics  Transonic flutter  Transonic speed  Wind tunnel tests  Wind-tunnel testing   A fast aeroelastic response prediction method based on proper orthogonal decomposition reduced order model 期刊论文 Yuhang Xuebao/Journal of Astronautics, 2009, 卷号: 30, 期号: 5, 页码: 1765-1769+1796 作者:  Chen, Gang;  Li, Yue-Ming;  Yan, Gui-Rong;  Xu, Min;  Zeng, Xian-Ang 收藏  |  浏览/下载：3/0  |  提交时间：2019/12/18 Aeroelastic dynamic response  Aeroelastic response  Aeroelastic system  Balanced truncation  Balanced truncation method  CFD/CSD  Computation efficiency  Coupled method  Coupled numerical simulation  Flutter boundaries  Frequency domains  Higher order  In-control  Numerical results  Order of magnitude  Proper orthogonal decompositions  Reduced order models  Time domain