40th AIAA Aerospace Sciences Meeting &Amp; Exhibit 2002
DOI: 10.2514/6.2002-122
|View full text |Cite
|
Sign up to set email alerts
|

Unstructured dynamic mesh for large movement and deformation

Abstract: In this paper, a simple robust method of the unstructured dynamic mesh for three-dimensional moving and deforming body problems is proposed. The method is developed to avoid the generation of squashed invalid elements by considering each elemental shape. With several three-dimensional applications, it is demonstrated that the present method significantly improves the robustness for problems with large motions of bodies without much penalty in CPU time. The use of the present method for grid movements on curved… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1

Citation Types

0
3
0

Year Published

2005
2005
2023
2023

Publication Types

Select...
9

Relationship

0
9

Authors

Journals

citations
Cited by 28 publications
(4 citation statements)
references
References 20 publications
0
3
0
Order By: Relevance
“…The double-layer absorber contains more detailed structural features, so the flow field shape is complex. The dynamic mesh method requires real-time reconstruction of the excessively distorted meshes in the changing flow field [46]. So, it is not realistic to numerically simulate the entire WEC with the existing computing resources in the laboratory, and this is also not necessary.…”
Section: Configuration Of Numerical Simulationsmentioning
confidence: 99%
“…The double-layer absorber contains more detailed structural features, so the flow field shape is complex. The dynamic mesh method requires real-time reconstruction of the excessively distorted meshes in the changing flow field [46]. So, it is not realistic to numerically simulate the entire WEC with the existing computing resources in the laboratory, and this is also not necessary.…”
Section: Configuration Of Numerical Simulationsmentioning
confidence: 99%
“…In the case of double-regulated turbines, a moving mesh is required for the runner blades as well. Various moving mesh methods have been employed for different industrial applications, such as the movement of the junction between the airplane tail and the fuselage [14] or free surface flows [15]. A transient numerical model of a pump-turbine was developed using a dynamic mesh method and re-meshing techniques in order to model the flow during load rejection [16].…”
Section: Introductionmentioning
confidence: 99%
“…Several smoothing methods are available, each with varying complexity and computational costs. Three commonly used methods include [34][35][36][37][38]: (i) elliptic mesh generation smoothing, such as the Laplacian smoothing [35,[39][40][41][42][43][44][45]; (ii) forced-based smoothing, using spring-like methods [34,46]; (iii) smoothing methods based on structural mechanics, such as elastic smoothing [36,37,47] (sometimes with the combination of the FEM Jacobian-based stiffening [48,49]) or hyperelastic smoothing [50][51][52].…”
mentioning
confidence: 99%