中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
机构
采集方式
内容类型
发表日期
学科主题
筛选

浏览/检索结果: 共8条,第1-8条 帮助

条数/页: 排序方式:
STRAIN TENSORS AND MATCHING PROPERTY ON DEGENERATED HYPERBOLIC SURFACES 期刊论文  OAI收割
SIAM JOURNAL ON MATHEMATICAL ANALYSIS, 2022, 卷号: 54, 期号: 4, 页码: 4930-4953
作者:  
Chen, Liang-Biao;  Yao, Peng-Fei
  |  收藏  |  浏览/下载:18/0  |  提交时间:2023/02/07
Strain tensors on hyperbolic surfaces and their applications 期刊论文  OAI收割
JOURNAL OF FUNCTIONAL ANALYSIS, 2021, 卷号: 281, 期号: 1, 页码: 36
作者:  
Yao, Peng-Fei
  |  收藏  |  浏览/下载:29/0  |  提交时间:2021/06/01
Lower Bounds of Optimal Exponentials of Thickness in Geometry Rigidity Inequality for Shells 期刊论文  OAI收割
JOURNAL OF SYSTEMS SCIENCE & COMPLEXITY, 2021, 页码: 17
作者:  
Yao Pengfei
  |  收藏  |  浏览/下载:20/0  |  提交时间:2021/04/26
The Time-Dependent Von Karman Shell Equation as a Limit of Three-Dimensional Nonlinear Elasticity 期刊论文  OAI收割
JOURNAL OF SYSTEMS SCIENCE & COMPLEXITY, 2020, 页码: 18
作者:  
Qin, Yizhao;  Yao, Peng-Fei
  |  收藏  |  浏览/下载:32/0  |  提交时间:2020/09/23
Optimal exponentials of thickness in Korn's inequalities for parabolic and elliptic shells 期刊论文  OAI收割
ANNALI DI MATEMATICA PURA ED APPLICATA, 2020, 页码: 23
作者:  
Yao, Peng-Fei
  |  收藏  |  浏览/下载:6/0  |  提交时间:2020/09/23
LINEAR STRAIN TENSORS ON HYPERBOLIC SURFACES AND ASYMPTOTIC THEORIES FOR THIN SHELLS 期刊论文  OAI收割
SIAM JOURNAL ON MATHEMATICAL ANALYSIS, 2019, 卷号: 51, 期号: 2, 页码: 1387-1435
作者:  
Yao, Peng-Fei
  |  收藏  |  浏览/下载:25/0  |  提交时间:2020/01/10
Development of nonlinear cross-anisotropic model for sands based on state parameter 期刊论文  OAI收割
JOURNAL OF CENTRAL SOUTH UNIVERSITY, 2013, 卷号: 20, 期号: 7, 页码: 1992-2000
作者:  
Chen Cheng;  Zhou Zheng-ming
  |  收藏  |  浏览/下载:13/0  |  提交时间:2018/06/05
A strong coupled CFD-CSD method on computational aeroelastity (EI CONFERENCE) 会议论文  OAI收割
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:67/0  |  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.