Development of Accelerated CFD/CSD Coupling Nonlinear Static Aeroelastic Algorithm Using Vortex Lattice Method

被引：0
|
作者：
Zou, Zhicheng [1 ]
Xie, Changchuan [1 ]
An, Chao [1 ]
Yang, Lan [2 ]
Ni, Zao [3 ]
机构：
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
[2] Beijing Inst Astronaut Syst Engn, Beijing 100076, Peoples R China
[3] Shanghai Aircraft Design & Res Inst, Loads & Flutter Dept, COMAC, Shanghai 201210, Peoples R China
来源：
AIAA JOURNAL | 2025年
关键词：
Aeroelastic Analysis; Civil Aircraft; Computational Fluid Dynamics; Numerical Analysis; Algorithm Design; RADIAL BASIS FUNCTIONS; MESH DEFORMATION;
D O I：
10.2514/1.J064826
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页数：6
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