This document provides information, guidelines, and practices for the application, use, and administration of two-dimensional and three-dimensional droplet impingement and ice accretion computer codes. The codes provide computational simulations of inflight icing that predict droplet trajectory, water loading, and ice accretion on aircraft components. These ice accretion characteristics are used during the aircraft design and certification process. ARP5903 has been reaffirmed to comply with the SAE five-year review policy.


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    Title :

    Droplet Impingement and Ice Accretion Computer Codes


    Publication date :

    2015-06-01



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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