This paper presents the results of a study designed to determine the level of fidelity required to accurately reproduce the performance effects of ice accretion on airfoils. Castings of streamwise and spanwise-ridge ice accretions were obtained from tests in an icing wind tunnel. The streamwise-ice accretion was characterized by a smooth conformal shape on the leading edge followed by rime feathers downstream. For the spanwise-ridge ice accretion the leading edge of the airfoil was smooth. There was an upper surface ridge at x/c = 0.10 and a lower surface ridge at x/c = 0.17. The high-fidelity casting simulations were attached to the leading edge of a subscale (457.2-mm (18-inch) chord) NACA 23012 model and aerodynamic performance testing was performed at a Reynolds number of 1.8×106 and a Mach number of 0.18. Lower-fidelity simulations were developed for each ice accretion to determine the fidelity required to match the performance of the airfoil with castings. For the streamwise ice, it was found that the addition of roughness to the lower-fidelity simulations was important to accurately model the aerodynamics. This paper reports the details of roughness size and concentration studies performed for the streamwise-ice simulations. It was found that the addition of roughness to the lower-fidelity simulations of the spanwise-ridge ice resulted in less aerodynamic fidelity. The flowfield associated with this ice shape was found to be highly three-dimensional, and therefore, very difficult to model with simple methods. This paper describes the flowfield and implications for aerodynamic simulation. The performance results are summarized and compared to previous work for horn-ice simulations.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Aerodynamic Fidelity of Ice Accretion Simulation on a Subscale Model


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    2007 SAE Aircraft and Engine Icing International Conference ; 2007



    Erscheinungsdatum :

    2007-09-24




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Aerodynamic Fidelity of Ice Accretion Simulation on a Subscale Model

    Broeren, A.P. / Busch, G.T. / Bragg, M.B. et al. | British Library Conference Proceedings | 2007


    Issues in Ice Accretion Aerodynamic Simulation on a Subscale Model

    Blumenthal, Leia / Busch, Greg / Broeren, Andy et al. | AIAA | 2006



    Aerodynamic Simulation of a Horn-Ice Accretion on a Subscale Model

    Busch, Greg / Broeren, Andy / Bragg, Michael | AIAA | 2007


    Aerodynamic Simulation of a Horn-Ice Accretion on a Subscale Model AIAA Paper

    Busch, G. / Broeren, A. / Bragg, M. et al. | British Library Conference Proceedings | 2007