A high-fidelity simulation model for icing effects flight training was developed from wind tunnel data for the DeHavilland DHC-6 Twin Otter aircraft. First, a flight model of the un-iced airplane was developed and then modifications were generated to model the icing conditions. The models were validated against data records from the NASA Twin Otter Icing Research flight test program with only minimal refinements being required. The goals of this program were to demonstrate the effectiveness of such a simulator for training pilots to recognize and recover from icing situations and to establish a process for modeling icing effects to be used for future training devices.


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    Title :

    Simulation Model Development for Icing Effects Flight Training


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    General Aviation Technology Conference & Exhibition ; 2002



    Publication date :

    2002-04-16




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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