Transonic Aeroelastic Numerical Simulation in Aeronautical Engineering | |
Yang GW(杨国伟) | |
刊名 | International Journal of Computational Fluid Dynamics,2006,20(5):339-347 |
2006 | |
通讯作者邮箱 | gwyang@imech.ac.cn |
ISSN号 | 1061-8562 |
通讯作者 | Yang, GW (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100080, Peoples R China. |
中文摘要 | A lower-upper symmetric Gauss-Seidel (LU-SGS) subiteration scheme is constructed for time-marching of the fluid equations. The Harten-Lax-van Leer-Einfeldt-Wada (HLLEW) scheme is used for the spatial discretization. The same subiteration formulation is applied directly to the structural equations of motion in generalized coordinates. Through subiteration between the fluid and structural equations, a fully implicit aeroelastic solver is obtained for the numerical simulation of fluid/structure interaction. To improve the ability for application to complex configurations, a multiblock grid is used for the flow field calculation and transfinite interpolation (TFI) is employed for the adaptive moving grid deformation. The infinite plate spline (IPS) and the principal of virtual work are utilized for the data transformation between the fluid and structure. The developed code was first validated through the comparison of experimental and computational results for the AGARD 445.6 standard aeroelastic wing. Then, the flutter character of a tail wing with control surface was analyzed. Finally, flutter boundaries of a complex aircraft configuration were predicted. |
学科主题 | 力学 |
类目[WOS] | Mechanics ; Physics, Fluids & Plasmas |
研究领域[WOS] | Mechanics ; Physics |
关键词[WOS] | NAVIER-STOKES EQUATIONS ; FLOW COMPUTATIONS ; WING FLUTTER |
收录类别 | SCI |
语种 | 英语 |
WOS记录号 | WOS:000241896300010 |
公开日期 | 2007-06-15 ; 2007-12-05 ; 2009-06-23 |
内容类型 | 期刊论文 |
源URL | [http://dspace.imech.ac.cn/handle/311007/16145] |
专题 | 力学研究所_力学所知识产出(1956-2008) |
推荐引用方式 GB/T 7714 | Yang GW. Transonic Aeroelastic Numerical Simulation in Aeronautical Engineering[J]. International Journal of Computational Fluid Dynamics,2006,20(5):339-347,2006. |
APA | 杨国伟.(2006).Transonic Aeroelastic Numerical Simulation in Aeronautical Engineering.International Journal of Computational Fluid Dynamics,2006,20(5):339-347. |
MLA | 杨国伟."Transonic Aeroelastic Numerical Simulation in Aeronautical Engineering".International Journal of Computational Fluid Dynamics,2006,20(5):339-347 (2006). |
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