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    Title :

    Effect of a Cutback Squealer and Cavity Depth on Film-Cooling Effectiveness for a Gas Turbine Blade Tip



    Conference:

    25th, Aerodynamic measurement technology and ground testing conference ; 2006 ; San Francisco, CA



    Publication date :

    2006-01-01


    Size :

    AIAA Paper 2006-3404-2006-3603


    Remarks:

    Including 25th AIAA aerodynamic measurement technology and ground testing conference 24th AIAA applied aerodynamics conference; 3rd AIAA flow control conference; 36th AIAA fluid dynamics conference and exhibit; 37th AIAA plasmadynamics and lasers conference; 9th AIAA/ASME joint thermophysics and heat transfer conference.; Paper numbers 2006-2805 to 2006-3925 with gaps held. Held on CD-ROM.; Shelved in Conference Index - see disc 11 for papers from the 25th Aerodynamic measurement technology and ground testing conference


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    Effect of a Cutback Squealer and Cavity Depth on Film-Cooling Effectiveness for a Gas Turbine Blade Tip

    Mhetras, Shantanu / Narzary, Diganta / Gao, Zhihong et al. | AIAA | 2006



    Film-Cooling Effectiveness on Squealer Cavity and Rim Walls of Gas-Turbine Blade Tip

    Shantanu Mhetras / Huitao Yang / Zhihong Gao et al. | AIAA | 2006


    Influence of tip clearance and cavity depth on heat transfer in a cutback squealer tip

    Wang, Weijie / Lu, Shaopeng / Jiang, Hongmei et al. | SAGE Publications | 2021