Abstract
A parallel program for the simulation of inviscid fluid flow around airfoils, based on the solution of unsteady Euler equations is presented. The concept of domain splitting and its connection with the selected parallelisation strategy is outlined. Furthermore, the implementation of the algorithm within the SUPRENUM environment as well as the treatment given to inter-process communication is also discussed. Finally, some topics about code development, use of simulation systems and preliminary validation test are quoted.
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