| dc.contributor.author | Mohd Zambri, Yusoff, Dr. | |
| dc.contributor.author | Ibrahim, Hussein, Prof. Dr. | |
| dc.contributor.author | Talal, Yusaf, Dr. | |
| dc.contributor.author | Zulkifli, Ahmad | |
| dc.date.accessioned | 2011-08-12T05:59:53Z | |
| dc.date.available | 2011-08-12T05:59:53Z | |
| dc.date.issued | 2005-09 | |
| dc.identifier.citation | The Journal of the Institution of Engineers, Malaysia, vol. 66(3), 2005, pages 14-20 | en_US |
| dc.identifier.issn | 0126-513X | |
| dc.identifier.uri | http://www.myiem.org.my/content/iem_journal_2005-176.aspx | |
| dc.identifier.uri | http://dspace.unimap.edu.my/123456789/13546 | |
| dc.description | Link to publisher's homepage at http://www.myiem.org.my/ | en_US |
| dc.description.abstract | A two-dimensional time-accurate time-marching viscous flow solver employing the viscous-inviscid interaction method
suitable for turbomachinery applications is described. The inviscid main flow solver uses the second-order accurate cellvertex
finite-volume spatial discretisation and fourth-order accurate Runge-Kutta temporal integration. The viscous effect due
to boundary layer development on the blade surfaces and wakes are modelled using an independent one-dimensional
boundary layer subroutine capable of modelling laminar, transition and fully turbulent flows. The solver has been applied to
subsonic, transonic and supersonic flow in a cascade of nozzle blades. The results are compared with the experimental data
and they showed very good agreement. | en_US |
| dc.language.iso | en | en_US |
| dc.publisher | The Institution of Engineers, Malaysia | en_US |
| dc.subject | Boundary layer | en_US |
| dc.subject | Computational Fluid Dynamics (CFD) | en_US |
| dc.subject | Time-marching | en_US |
| dc.subject | Turbine | en_US |
| dc.subject | Turbomachinery | en_US |
| dc.subject | Viscous | en_US |
| dc.title | Modeling of viscous flows in two-dimensional turbomachinery cascade via viscous-inviscid interaction method | en_US |
| dc.type | Article | en_US |
