Please use this identifier to cite or link to this item: https://doi.org/10.1016/j.jcp.2009.11.037
DC FieldValue
dc.titleSVD-GFD scheme to simulate complex moving body problems in 3D space
dc.contributor.authorWang, X.Y.
dc.contributor.authorYu, P.
dc.contributor.authorYeo, K.S.
dc.contributor.authorKhoo, B.C.
dc.date.accessioned2014-06-17T06:35:11Z
dc.date.available2014-06-17T06:35:11Z
dc.date.issued2010-03-20
dc.identifier.citationWang, X.Y., Yu, P., Yeo, K.S., Khoo, B.C. (2010-03-20). SVD-GFD scheme to simulate complex moving body problems in 3D space. Journal of Computational Physics 229 (6) : 2314-2338. ScholarBank@NUS Repository. https://doi.org/10.1016/j.jcp.2009.11.037
dc.identifier.issn00219991
dc.identifier.urihttp://scholarbank.nus.edu.sg/handle/10635/61442
dc.description.abstractThe present paper presents a hybrid meshfree-and-Cartesian grid method for simulating moving body incompressible viscous flow problems in 3D space. The method combines the merits of cost-efficient and accurate conventional finite difference approximations on Cartesian grids with the geometric freedom of generalized finite difference (GFD) approximations on meshfree grids. Error minimization in GFD is carried out by singular value decomposition (SVD). The Arbitrary Lagrangian-Eulerian (ALE) form of the Navier-Stokes equations on convecting nodes is integrated by a fractional-step projection method. The present hybrid grid method employs a relatively simple mode of nodal administration. Nevertheless, it has the geometrical flexibility of unstructured mesh-based finite-volume and finite element methods. Boundary conditions are precisely implemented on boundary nodes without interpolation. The present scheme is validated by a moving patch consistency test as well as against published results for 3D moving body problems. Finally, the method is applied on low-Reynolds number flapping wing applications, where large boundary motions are involved. The present study demonstrates the potential of the present hybrid meshfree-and-Cartesian grid scheme for solving complex moving body problems in 3D. © 2009 Elsevier Inc. All rights reserved.
dc.description.urihttp://libproxy1.nus.edu.sg/login?url=http://dx.doi.org/10.1016/j.jcp.2009.11.037
dc.sourceScopus
dc.subjectFlapping wings
dc.subjectGeneralized finite difference
dc.subjectHybrid meshfree-and-Cartesian grid
dc.subjectIncompressible Navier-Stokes
dc.subjectMoving body
dc.typeArticle
dc.contributor.departmentMECHANICAL ENGINEERING
dc.description.doi10.1016/j.jcp.2009.11.037
dc.description.sourcetitleJournal of Computational Physics
dc.description.volume229
dc.description.issue6
dc.description.page2314-2338
dc.description.codenJCTPA
dc.identifier.isiut000275092000021
Appears in Collections:Staff Publications

Show simple item record
Files in This Item:
There are no files associated with this item.

Google ScholarTM

Check

Altmetric


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.