Abstract This paper reports the results of an experimental study of heat transfer using a model of the internal cooled surface of the turbine blade leading edge. We investigated a joint action of air jets and hemispherical protrusions on heat transfer from the concave surface of the leading edge model to air.


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    Title :

    Heat transfer enhancement in combined cooling of the turbine blade leading edge


    Contributors:

    Published in:

    Publication date :

    2013-10-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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