Siva Kumar, K and Sharanappa, Sajjan V (2012) Unsteady Flow past a Flapping Aerofoil. TRANSACTION ON CONTROL AND MECHANICAL SYSTEMS, 1 (1). pp. 43-48.
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Official URL: http://tsest.org/index.php/TCMS/article/view/29/10
Abstract
Abstract: Unsteady flow computations are presented for low speed Mach number flow past a combined pitching and plunging aerofoil. The Implicit Reynolds-averaged Navier-Stokes solver used for obtaining time-accurate solutions is based on finite volume nodal point spatial discretization scheme with dual time stepping. Results are obtained in the form of aerodynamic coefficients, time – averaged thrust coefficient and propulsion efficiency which agree well with the available results.
| Item Type: | Article |
|---|---|
| Subjects: | AERONAUTICS > Aerodynamics ENGINEERING > Fluid Mechanics and Thermodynamics |
| Depositing User: | Mr. Sharanappa V. Sajjan |
| Date Deposited: | 26 Jun 2013 09:53 |
| Last Modified: | 26 Jun 2013 09:53 |
| URI: | http://nal-ir.nal.res.in/id/eprint/11722 |
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