Scheme for numerical simulation of transonic, compressible, viscous flow about two-dimensional cascade of oscillating rigid airfoils involves finite-difference solution of Navier-Stokes equations on coordinate grid deforming with motions of airfoils. Contributes to understanding of flows around advanced turboprop airfoil sections. Cascade represented by periodic grid conforming to airfoils and to outer boundaries. Oscillation of airfoil represented by deformation of grid. Applications of deforming-grid technique includes turbomachinery and aeroelastic modeling of nonrigid airfoils.


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    Titel :

    Navier-Stokes Calculations With Deforming Grid


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1989-07-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



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    Special Issues in Unsteady Navier-Stokes Simulations with Deforming Bodies

    Hoffren, J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences | British Library Conference Proceedings | 1996


    Special Issues in Unsteady Navier-Stokes Simulations with Deforming Bodies

    Hoffren, J. | British Library Online Contents | 1996