Agglomeration Multigrid Solutions of Laminar Viscous Flows
نویسندگان
چکیده
The paper describes the implementation details and validation results for an agglomeration multigrid procedure developed in the context of hybrid, unstructured grid solutions of aerodynamic flows. The procedure is applied to the solution of 2-D, laminar viscous flows of aerospace interest. The governing equations are discretized with an unstructured grid finite volume method which is capable of handling hybrid unstructured grids. Time march uses an explicit, 5-stage, Runge-Kutta time-stepping scheme. Convergence acceleration to steady state is achieved through the implementation of an agglomeration multigrid procedure which retains all the flexibility previously available in the unstructured grid code. The calculation capability created is applied to 2-D laminar viscous flows of aerospace interest. Studies of the various parameters affecting the multigrid acceleration performance are undertaken with the objective of determining optimal numerical parameter combinations.
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