Anand, kumar (1988) Euler solutions with a multi-block structured code 13; 13;. Journal of Aeronautical Society of India, 40. pp. 89-95.
Full text not available from this repository.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: | Article |
|---|---|
| Uncontrolled Keywords: | Computational fluid dynamics;Euler equations of motion;Grid generation(mathematics);Delta wings;Flow equations;Roots of equations;Vortices |
| Subjects: | AERONAUTICS > Aerodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 13 Oct 2006 |
| Last Modified: | 05 Aug 2015 09:01 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2973 |
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