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    Thermal Fatigue Life Prediction of Air-Cooled Gas Turbine Vanes 

    Source: Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 002:;page 414
    Author(s): T. Sato; K. Takeishi; T. Sakon
    Publisher: The American Society of Mechanical Engineers (ASME)
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    An Experimental Study of Heat Transfer and Film Cooling on Low Aspect Ratio Turbine Nozzles 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003:;page 488
    Author(s): K. Takeishi; M. Matsuura; S. Aoki; T. Sato
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of the three-dimensional flow field on the heat transfer and the film cooling on the endwall, suction, and pressure surface of an airfoil were studied using a low speed, fully ...
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    Film Cooling on a Gas Turbine Rotor Blade 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 004:;page 828
    Author(s): K. Takeishi; K. Tsukagoshi; S. Aoki; T. Sato
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The film cooling effectiveness on a low-speed stationary cascade and the rotating blade has been measured by using a heat-mass transfer analogy. The film cooling effectiveness on the suction ...
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    Study on the Turbine Vane and Blade for a 1500°C Class Industrial Gas Turbine 

    Source: Journal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 003:;page 597
    Author(s): S. Amagasa; K. Takeishi; S. Aoki; K. Aoyama; H. Kawai; K. Shimomura; M. Kadowaki
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the summary of a three-year development program for the first-stage stationary vane and rotating blade for the next generation, 1500°C class, high-efficiency gas turbine. ...
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