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    Prediction of Film Cooling by a Row of Holes With a Two-Dimensional Boundary-Layer Procedure 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 004:;page 579
    Author(s): B. Schönung; W. Rodi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present paper describes predictions of film cooling by a row of holes. The calculations have been performed by a two-dimensional boundary-layer code with special modifications that account ...
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    Systematic Study of Film Cooling With a Three-Dimensional Calculation Procedure 

    Source: Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 001:;page 124
    Author(s): A. O. Demuren; W. Rodi; B. Schönung
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present paper describes three-dimensional calculations of film cooling by injection from a single row of holes. A systematic study of the influence of different parameters on the cooling ...
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    The Influence of Density Difference Between Hot and Coolant Gas on Film Cooling by a Row of Holes: Predictions and Experiments 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 004:;page 747
    Author(s): W. Haas; W. Rodi; B. Schönung
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The two-dimensional boundary-layer procedure of Schönung and Rodi [1] for calculating film cooling by a row of holes was extended to account for density differences between hot gas and injected ...
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    Calculation of Wake-Induced Unsteady Flow in a Turbine Cascade 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 004:;page 675
    Author(s): N.-H. Cho; X. Liu; W. Rodi; B. Schönung
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Numerical predictions are reported for two-dimensional unsteady flow in a linear turbine cascade, where the unsteadiness is caused by passing wakes generated by the preceding row of blades. In ...
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