An experiment was conducted in the Icing Research Tunnel (IRT) at NASA Glenn Research Center to study the effect of sweep angle and temperature on the formation of ice accretions on a NACA 0012 swept wing at SLD conditions. From a baseline Appendix-C condition with a MVD of 20m the drop size was changed to 110 and 200m for the SLD cases. Casting data, ice shape tracings, time-sequence and photographic data were obtained. Time-sequence photography was taken during each run to capture in real time the formation of the ice accretion. Measurements of the critical distance were obtained.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Parametric Study of Ice Accretion Formation on a Swept Wing at SLD Conditions


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Tsao, Jen-Ching (Autor:in) / Vargas, Mario (Autor:in)

    Kongress:

    2007 SAE Aircraft and Engine Icing International Conference ; 2007



    Erscheinungsdatum :

    2007-09-24




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Parametric Study of Ice Accretion Formation on a Swept Wing at SLD Conditions

    Vargas, M. / Tsao, J.-C. / Society of Automotive Engineers | British Library Conference Proceedings | 2007


    Swept wing ice accretion modeling

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


    Swept-Wing Ice Accretion Characterization and Aerodynamics

    A. P. Broeren / M. G. Potapczuk / J. T. Riley et al. | NTIS | 2013


    Swept-Wing Ice Accretion Characterization and Aerodynamics

    Broeren, Andy P. / Potapczuk, Mark / Riley, James et al. | AIAA | 2013


    Swept-Wing Ice Accretion Characterization and Aerodynamics

    Broeren, Andy P. / Potapczuk, Mark G. / Riley, James T. et al. | NTRS | 2013