Application of method of false transients to generate smooth grids around a body in motion
DOI:
https://doi.org/10.21914/anziamj.v50i0.1425Abstract
A time marching finite difference scheme incorporating an efficient method of false transients, an approximate factorisation technique and a time steps cycling process, is presented for solution of a system of Poisson's equations. The solution to the equations provides a smooth three dimensional boundary fitted grid around a body in motion. The scheme required much less computational effort than that required by other iterative schemes. In closure, examples of a static grid around an aircraft tailplane and a dynamic grid around a flapping wing are presented. References- Ly, E., Improved Approximate Factorisation Algorithm for the Steady Subsonic and Transonic Flow over an Aircraft Wing, in Proceedings of the 21st Congress of the International Council of the Aeronautical Sciences (ICAS98), AIAA and ICAS, Melbourne, Australia, Sep. 1998, Paper A98-31699.
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Published
2008-12-05
Issue
Section
Proceedings Computational Techniques and Applications Conference