An Investigation into the Convergence of the AF-CGS method. G.U. Aero Report 9327

Glover, I.C. (1993) An Investigation into the Convergence of the AF-CGS method. G.U. Aero Report 9327. Technical Report. Department of Aerospace Engineering, University of Glasgow.

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Abstract

The relationship between the relative residual produced by the AFCGS method and the lift, drag and pressure coefficients is investigated for steady turbulent flow over a NACA64A010 aerofoil, and over an RAE2822 aerofoil. This enables the most suitable convergence criterion to be established.

Item Type:Research Reports or Papers (Technical Report)
Status:Published
Glasgow Author(s) Enlighten ID:UNSPECIFIED
Authors: Glover, I.C.
College/School:College of Science and Engineering > School of Engineering > Aerospace Sciences
Publisher:Department of Aerospace Engineering, University of Glasgow
Copyright Holders:Copyright © 1993 Department of Aerospace Engineering, University of Glasgow
Publisher Policy:Reproduced with the permission of the Department

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