Saxena, SK and Nair, Manoj T (2004) Development and Critical Assessment of Technology for Numerical Simulation of Hypersonic Real Gas Flows. Project Report. National Aerospace Laboratories, Bangalore, India.
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Abstract
This paper provides details of the Reynolds Averaged Navier-Stokes (RANS) equations based Computational Fluid Dynamics (CFD) technology developed for numerical simulation of hypersonic real gas flows. Numerical and physical aspects of such a simulation are emphasized to bring out the challenges involved. Results of validation of the RANS code on a standard configuration for which experimental data is available are discussed.
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Real gas, chemical non-equilibrium, hypersonic flow, RANS |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division |
| Depositing User: | MS Jayashree S |
| Date Deposited: | 24 Jan 2005 |
| Last Modified: | 24 May 2010 09:39 |
| URI: | http://nal-ir.nal.res.in/id/eprint/579 |
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