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    Experimental and Numerical Investigation on the Evaporation of Shear-Driven Multicomponent Liquid Wall Films 

    Source: Journal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;issue: 003:;page 580
    Author(s): M. Gerendas; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The presented work is concerned with two-phase flows similar to those in prefilming airblast atomizers and combustors employing film vaporization. Correlations for the multicomponent mixture ...
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    Impact of Swirl Flow on the Cooling Performance of an Effusion Cooled Combustor Liner 

    Source: Journal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 012:;page 121503
    Author(s): B. Wurm; A. Schulz; H.-J. Bauer; M. Gerendas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental study on combustor liner cooling of modern direct lean injection combustion chambers using coolant ejection from both effusion cooling holes and a starter film has been conducted. ...
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    Droplet Entrainment From a Shear-Driven Liquid Wall Film in Inclined Ducts: Experimental Study and Correlation Comparison 

    Source: Journal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 004:;page 874
    Author(s): J. Ebner; M. Gerendás; O. Schäfer; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The primary objective of the present study is to clarify the droplet disintegration mechanism and the film properties of liquid oil films driven by shear stress, which is induced by a co-current ...
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    A Combined Finite Element-Multiple Criteria Optimization Approach for Materials Selection of Gas Turbine Components 

    Source: Journal of Applied Mechanics:;2012:;volume( 079 ):;issue: 006:;page 61019
    Author(s): A. Shanian; A. S. Milani; N. Vermaak; K. Bertoldi; T. Scarinci; M. Gerendas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The design of critical components for aerospace applications involves a number of conflicting functional requirements: reducing fuel consumption, cost, and weight, while enhancing performance, ...
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