Unsteady Flow past a Flapping Aerofoil

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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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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