Saxena, SK (1992) An upwind formulation for the solution of thin-layer Navier-stokes equations. Journal of Aeronautical Society of India, 44 (3). pp. 253-257.
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Abstract
Thin-Layer Navier-Stokes equations in generalized body-fitted coordinate system and non-dimensional form are solved to numerically simulate high speed viscous flows.13; A second order accurate explicit upwind MUSCL type algorithm incorporating flux-vector splitting due to Van Leer is formulated within the frame work to finite volume13; approach. TVD limiters are used to avoid undershoots and overshoots in the skock region. The results of laminar flow calculations are presented for hemisphere cylinder13; configuration at supersonic Mach number.
| Item Type: | Article |
|---|---|
| Uncontrolled Keywords: | Navier-stokes equation;Thin layer |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics |
| Depositing User: | Mr. Ravikumar R |
| Date Deposited: | 10 Oct 2006 |
| Last Modified: | 24 May 2010 04:21 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2947 |
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