A study is made following with computational analysis of the effect of icing when it forms on the wing of an aircraft. This computational analysis based model includes an entire wing segment whose airfoil distorts due to the formation of ice along the leading edge, all efforts directed towards the assessment and determination of the effects of this system on flight performance. This analysis will help us to understand the importance of anti-icing system for an aircraft


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    Title :

    Computational analysis of Anti icing system of an aircraft wing


    Contributors:


    Publication date :

    2019-06-01


    Size :

    3270979 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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