Dutta, Vimala and Dutta, PK and Sajjan, SV (2008) RANS Computations for flow through a variable mach number flexible nozzle at a mach 4. In: Proceedings of the International Conference on Aerospace Science and Technology (INCAST 2008-056), 26-28 Jun 2008, Bangalore, India.
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) |
PDF
INCAST_2008-056.pdf Download (323kB) |
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/other.png) |
Indexer Terms (Generate index codes conversion from application/pdf to indexcodes)
indexcodes.txt Download (4kB) |
Abstract
Numerical simulation of flow through a Variable Mach number Flexible Nozzle (VMFN) at Mach 4 is carried out using the CFD code IMPRANS to validate the design of the nozzle based on the method of characteristics with boundary layer correction. The CFD analysis for the contour uses an implicit Reynolds-averaged Navier-Stokes (RANS) solver with Baldwin-Lomax turbulence model.Detailed flow characteristics like the centerline Mach number distribution and Mach contours of the steady flow through the converging x2013; diverging nozzle are obtained to study and assess the suitability of the design.
| Item Type: | Conference or Workshop Item (Paper) |
|---|---|
| Additional Information: | Copyright for this article belongs to National Aerospace Laboratories |
| Uncontrolled Keywords: | Reynolds-averaged Navier-Stokes (RANS);Flux vectors;RANS computations |
| Subjects: | AERONAUTICS > Aeronautics (General) |
| Depositing User: | Ms. Alphones Mary |
| Date Deposited: | 06 Mar 2009 |
| Last Modified: | 17 Jun 2010 09:02 |
| URI: | http://nal-ir.nal.res.in/id/eprint/5006 |
Actions (login required)
 |
View Item |
