The multigrid method is applied to the calculation of transonic, potential flow fields about arbitrary three dimensional wing-body combinations. Numerical results for iterative convergence rate are in good agreement with those predicted by a local mode analysis and show substantial improvement over conventional relaxation algorithms.


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    Title :

    Applications of the multigrid method to calculations of transonic potential flow about wing fuselage combinations


    Contributors:


    Publication date :

    1981-10-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English