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Research on Bottom Drag Prevention for an Unmanned Deepwater Collection 会议论文
PROCEEDINGS OF 2018 IEEE 3RD ADVANCED INFORMATION TECHNOLOGY, ELECTRONIC AND AUTOMATION CONTROL CONFERENCE (IAEAC 2018), 2018-01-01
作者:  Xiao, Yu-long[1];  Zhu, Chuan[2];  Yao, Jun-feng[3];  Peng, Yan[4];  Yang, Gui-geng[5]
收藏  |  浏览/下载：9/0  |  提交时间：2019/04/22
Review and comparison of empirical thermospheric mass density models 期刊论文
Progress in Aerospace Sciences, 2018, 卷号: Vol.103, 页码: 31-51
作者:  Changyong He;  Yang Yang;  Brett Carter;  Emma Kerr;  Suqin Wu
收藏  |  浏览/下载：3/0  |  提交时间：2019/12/26
Flap upward deflection and rearward bump combination to alleviate transonic buffet of supercritical wing 会议论文
AIAA Aerospace Sciences Meeting, 2018, 2018-01-08
作者:  Gao, S.;  Yun, T.;  Liu, P.;  Qu, Q.
收藏  |  浏览/下载：12/0  |  提交时间：2019/12/30
Comparison of drag prediction using RANS models and DDES for the DLR-F6 configuration using high order schemes 会议论文
54th AIAA Aerospace Sciences Meeting, 2016, San Diego, CA, United states, January 4, 2016 - January 8, 2016
作者:  Gan JY;  Shen YQ(申义庆);  Zha GC
收藏  |  浏览/下载：17/0  |  提交时间：2017/05/05
Finite Element Method for Simulating the Effects of Torque and Drag On Buckling of Tubular inside Borehole of an Oil and Gas Wells 会议论文
International Conference on Advanced Material and Manufacturing Science (ICAMMS 2012), Beijing, PEOPLES R CHINA, 2014-01-01
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收藏  |  浏览/下载：3/0  |  提交时间：2020/01/03
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：62/0  |  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.  
The wear and drag prediction of the 2D micro-asperities on textured wall 会议论文
作者:  Traore, Moussa Magara;  Li, Wang
收藏  |  浏览/下载：1/0  |  提交时间：2019/12/10
Study on the Reynolds stress modele for drag reducing viscoelastic flows 期刊论文
Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2009, 卷号: 30, 期号: 4, 页码: 611-614
作者:  Wang, Yi;  Yu, Bo;  Zhang, Jin-Jun;  Wei, Jin-Jia;  Zhang, Hong-Na
收藏  |  浏览/下载：9/0  |  提交时间：2019/12/18

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