Simulated glaze ice accretion effects on a flowfield are presently studied for the case of a 3D semispan wing with NACA 0012 airfoil section on a rectangular untwisted planform. The model was tested at both zero-sweep and 30-deg sweep setting with four-beam/two-color LDV flowfield mapping. The comparison of LDV-measure velocity profiles with 3D Navier-Stokes predictions revealed correct trends, but with several differences that are attributable to the turbulence models and grid resolution used in the computations.


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    Titel :

    LDV flowfield measurements on a straight and swept wing with a simulated ice accretion


    Beteiligte:
    Bragg, M. B. (Autor:in) / Kerho, M. F. (Autor:in) / Khodadoust, A. (Autor:in)

    Kongress:

    AIAA, Aerospace Sciences Meeting and Exhibit ; 1993 ; Reno, NV, United States


    Erscheinungsdatum :

    01.01.1993


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Vortical Flowfield Structure at Forward Swept-Wing Configurations

    Christian Breitsamter / Boris Laschka | AIAA | 2001



    Swept wing ice accretion modeling

    POTAPCZUK, M. / BIDWELL, C. | AIAA | 1990