Srikanth, VC and Mujumdar, Sekhar (1992) Relative performance of different low reynolds number turbulence models for prediction of fully developed channel13; flow. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Full text available as:![[img]](http://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) | PDF Restricted to Archive staff only Download (1949Kb) |
Abstract
An existing code for calculation of Turbulent, Incompressible flow for complex geometries properties13; using k- E model is modified for prediction of turbulent13; to run with a Low Reynolds number version of the k- 6 model. The code which was -using Wall Functions has been for calculation of near-wall properties modified suitably with the Low Reynolds been near-wall number version to obtain more accurate in a plane 2D has quantities. chosen as the Flow channel test case with periodic boundary conditions. The results of five different Low Reynolds Numerical number version are compared with Direct Simulation-results . The computation domain of the channel has 5x80 control volumes with a stretching factor of 1 .05 in the transverse direction.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Two equation turbulence model;K-eturbulence model;Near wall effects;Finite volume method;Flow incompressible |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics AERONAUTICS > Aeronautics (General) |
| Division/Department: | Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division |
| Depositing User: | Mr. N A |
| Date Deposited: | 11 Jul 2006 |
| Last Modified: | 24 May 2010 09:43 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1730 |
Actions (login required)
| View Item |
