Euler solutions with a multi-block structured code 13; 13;

Anand, kumar (1988) Euler solutions with a multi-block structured code 13; 13;. Journal of Aeronautical Society of India, 40 . pp. 89-95.

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Abstract

Multiblock schemes enhance the scope of application of computational fluid dynamics to present-day complex configurations. With multiblock grid generation, embedded grids, and different equations in different domains, it should be possible to resolve the main features of flow over a complete aircraft with a grid containing about a million cells. Basic steps in the coding of multiblock schemes are described. Euler solutions for the vortex- dominated flow over a cropped delta wing are presented. These solutions show separation from the leading edge and formation of a leeside vortex. (B.J.)

Item Type: Journal Article
Uncontrolled Keywords: Computational fluid dynamics;Euler equations of motion;Grid generation(mathematics);Delta wings;Flow equations;Roots of equations;Vortices
Subjects: AERONAUTICS > Aerodynamics
Division/Department: Fluid Dynamics
Depositing User: M/S ICAST NAL
Date Deposited: 13 Oct 2006
Last Modified: 24 May 2010 09:51
URI: http://nal-ir.nal.res.in/id/eprint/2973

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