Chakrabartty, SK (1992) Approximate factorization scheme for transonic potential flow computations. Sadhana, 17 (2). pp. 299-313. ISSN 0256-2499
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Abstract
The implicit approximate factorization scheme known as AF2 is investigated for application to the solution of two- and three-dimensional transonic full potential equations in conservative form. The artificial viscosity used by different authors has been deduced, and is discussed in detail. A second-order correction to the implicit artificial viscosity is tested for transonic flow past a Korn aerofoil at both design and off-design conditions. The inviscid transonic flow past different aerofoils, wings, and wing-body configurations has been computed using the AF2 scheme, and the solutions are compared with experimental and other numerical results. It is shown that the AF2 scheme is fast, and is not sensitive to grid stretching
| Item Type: | Journal Article |
|---|---|
| Additional Information: | Copyright for this article belongs to Indian Academy of Sciences |
| Uncontrolled Keywords: | Aerospace computing;Transonic flow;Viscosity of gases; Transonic potential flow computations;Implicit approximate factorization scheme;Artificial viscosity;Second-order correction;Inviscid flow |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics |
| Division/Department: | Computational and Theoretical Fluid Dynamics Division |
| Depositing User: | MS Jayashree S |
| Date Deposited: | 15 Apr 2008 |
| Last Modified: | 24 May 2010 09:55 |
| URI: | http://nal-ir.nal.res.in/id/eprint/4172 |
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