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    Experimental Investigation of Secondary Flow Structure in a Blade Passage With and Without Leading Edge Fillets 

    Source: Journal of Fluids Engineering:;2007:;volume( 129 ):;issue: 003:;page 253
    Author(s): G. I. Mahmood; S. Acharya
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Velocity and pressure measurements are presented for a blade passage with and without leading edge contouring in a low speed linear cascade. The contouring is achieved through fillets placed ...
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    Spatially Resolved Heat Transfer and Friction Factors in a Rectangular Channel With 45-Deg Angled Crossed-Rib Turbulators 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 003:;page 575
    Author(s): P. M. Ligrani; G. I. Mahmood
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Spatially resolved Nusselt numbers, spatially averaged Nusselt numbers, and friction factors are presented for a stationary channel with an aspect ratio of 4 and angled rib turbulators inclined ...
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    Local Heat Transfer and Flow Structure on and Above a Dimpled Surface in a Channel 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 001:;page 115
    Author(s): G. I. Mahmood; H.-K. Moon; Consulting Engineer; B. Glezer; Head; Turbine Cooling and Heat Transfer Analysis; M. L. Hill; D. L. Nelson; P. M. Ligrani; Professor.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental results, measured on and above a dimpled test surface placed on one wall of a channel, are given for Reynolds numbers from 1250 to 61,500 and ratios of air inlet stagnation ...
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