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    Characterization and Laboratory Simulation of Turbine Airfoil Surface Roughness and Associated Heat Transfer 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 002:;page 337
    Author(s): D. G. Bogard; M. Tabbita; D. L. Schmidt
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The physical characteristics of surface roughness observed on first-stage high-pressure turbine vanes that had been in service for a long period were investigated in this study. Profilometry ...
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    Film Cooling With Compound Angle Holes: Heat Transfer 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 004:;page 800
    Author(s): B. Sen; D. L. Schmidt; D. G. Bogard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Heat transfer coefficients have been measured for film cooling injection from a single row of holes laterally directed with a compound angle of 60 deg. Two hole configurations were tested, ...
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    Film Cooling With Compound Angle Holes: Adiabatic Effectiveness 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 004:;page 807
    Author(s): D. L. Schmidt; B. Sen; D. G. Bogard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Film cooling effectiveness was studied experimentally in a flat plate test facility with zero pressure gradient using a single row of inclined holes, which injected high-density, cryogenically ...
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