Publication: Multigrid solution of Euler equations using high-resolution NVD differencing scheme for unstructured meshes
| dc.citedby | 9 | |
| dc.contributor.author | Ng K.C. | en_US |
| dc.contributor.author | Yusoff M.Z. | en_US |
| dc.contributor.author | Ng E.Y.K. | en_US |
| dc.contributor.authorid | 55310814500 | en_US |
| dc.contributor.authorid | 7003976733 | en_US |
| dc.contributor.authorid | 7201647536 | en_US |
| dc.date.accessioned | 2023-12-28T08:57:36Z | |
| dc.date.available | 2023-12-28T08:57:36Z | |
| dc.date.issued | 2006 | |
| dc.description.abstract | High-speed compressible flows in a nozzle and over an airfoil have been computed by solving the Euler equations using the GAMMA differencing scheme for spatial discretisation on unstructured grid. This high-resolution technique originally developed in a segregated algorithm has now been modified for the present coupled solver by introducing a non-linear blending factor to enhance its convergence property while preserving the Total Variation Diminishing (TVD) criterion. The efficiencies of the GAMMA scheme and its variant have been augmented with a novel agglomeration multigrid scheme to accelerate the convergence to steady state using the multi-stage Runge-Kutta time-marching technique. Copyright � 2006 Inderscience Enterprises Ltd. | en_US |
| dc.description.nature | Final | en_US |
| dc.identifier.doi | 10.1504/PCFD.2006.010964 | |
| dc.identifier.epage | 401 | |
| dc.identifier.issue | 7 | |
| dc.identifier.scopus | 2-s2.0-33845511110 | |
| dc.identifier.spage | 389 | |
| dc.identifier.uri | https://www.scopus.com/inward/record.uri?eid=2-s2.0-33845511110&doi=10.1504%2fPCFD.2006.010964&partnerID=40&md5=230148dd3bbb5503add5879741509d6e | |
| dc.identifier.uri | https://irepository.uniten.edu.my/handle/123456789/29770 | |
| dc.identifier.volume | 6 | |
| dc.pagecount | 12 | |
| dc.publisher | Inderscience Publishers | en_US |
| dc.source | Scopus | |
| dc.sourcetitle | Progress in Computational Fluid Dynamics | |
| dc.subject | Agglomeration multigrid | |
| dc.subject | Compressible flow | |
| dc.subject | Density-based method | |
| dc.subject | GAMMA scheme | |
| dc.subject | Normalised Variable Diagram (NVD) | |
| dc.subject | Unstructured mesh | |
| dc.subject | Airfoils | |
| dc.subject | Algorithms | |
| dc.subject | Compressible flow | |
| dc.subject | Computational fluid dynamics | |
| dc.subject | Computer simulation | |
| dc.subject | Convergence of numerical methods | |
| dc.subject | Nozzles | |
| dc.subject | Runge Kutta methods | |
| dc.subject | Airfoils | |
| dc.subject | Algorithms | |
| dc.subject | Compressible flow | |
| dc.subject | Computer simulation | |
| dc.subject | Convergence of numerical methods | |
| dc.subject | Nozzles | |
| dc.subject | Runge Kutta methods | |
| dc.subject | Agglomeration multigrid scheme | |
| dc.subject | Euler equations | |
| dc.subject | GAMMA differencing scheme | |
| dc.subject | Normalised Variable Diagram (NVD) | |
| dc.subject | Unstructured mesh | |
| dc.subject | Computational fluid dynamics | |
| dc.title | Multigrid solution of Euler equations using high-resolution NVD differencing scheme for unstructured meshes | en_US |
| dc.type | Article | en_US |
| dspace.entity.type | Publication |