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- W85800670 abstract "Unsteady flow over an aerofoil undergoing flappingmotion has been carried out numerically in order to assess the effect of aerofoil thickness and camber on the aerodynamic performance using an in-house developed implicit Reynolds averaged Navier-Stokes solver IMPRANS. The solver is based on a finite volume nodal point spatial discretization scheme for compressible viscous flows with dual time stepping. The algebraic eddy viscosity model due to Baldwin and Lomax is used for the turbulence closure. The results are obtained in the form of aerodynamic coefficients, thrust coefficient and propulsion efficiency." @default.
- W85800670 created "2016-06-24" @default.
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- W85800670 date "2013-11-21" @default.
- W85800670 modified "2023-09-26" @default.
- W85800670 title "Effect of Aerofoil Thickness and Camber on the Flapping Aerofoil Propulsion" @default.
- W85800670 hasPublicationYear "2013" @default.
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