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    Title :

    Jet Diameter Effect on Impingement Jet Cooling on the Leading Edge of a Turbine Blade


    Contributors:

    Conference:

    54th AIAA Aerospace Sciences Meeting



    Publication date :

    2016-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Jet Diameter Effect on Impingement Jet Cooling on the Leading Edge of a Turbine Blade (AIAA 2016-0905)

    Haider, Syed A. / Yan, X. Terry | British Library Conference Proceedings | 2016


    Numerical Study on Flow and Heat Transfer of Impingement Cooling on Leading Edge of Actual Turbine Blade

    Liu, Z. / Feng, Z. / Song, L. | British Library Online Contents | 2011


    Stagnation Region Gas Film Cooling for Turbine Blade Leading-Edge Applications

    D.W. Luckey / D.K. Winstanley / G.J. Hanus et al. | AIAA | 1977


    Stagnation region gas film cooling for turbine blade leading edge applications

    LUCKEY, D. / WINSTANLEY, D. / HANUS, G. et al. | AIAA | 1976