Khan, AA and Shembharkar, TR (2008) Viscous flow analysis in a convergent-divergent nozzle. In: Proceedings of the International Conference on Aerospace Science and Technology, 26-28 Jun 2008, Bangalore, India.
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Abstract
The classical one-dimensional inviscid theory does not reveal the complex flow features in a choked CD nozzle accurately. The code Fluent has been used to compute RANS flow in a 2-D CD13; nozzle for nozzle pressure ratios (NPR) corresponding to presence of shock inside the diverging part of the13; nozzle. The computed solutions differ from the simple theory so far as shock location, shock structure and13; after-shocks are concerned.
| Item Type: | Conference or Workshop Item (Paper) |
|---|---|
| Additional Information: | Copyright for this article belongs to National Aerospace Laboratories |
| Uncontrolled Keywords: | Viscous flow;Nozzle pressure ratios (NPR);Shock structure |
| Subjects: | AERONAUTICS > Aeronautics (General) |
| Division/Department: | Propulsion Division, Propulsion Division |
| Depositing User: | Ms. Alphones Mary |
| Date Deposited: | 20 Feb 2009 |
| Last Modified: | 17 Jun 2010 14:15 |
| URI: | http://nal-ir.nal.res.in/id/eprint/4982 |
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