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    Calculation Approach Validation for Airblast Atomizers 

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002:;page 386
    Author(s): N. K. Rizk; H. C. Mongia
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In order to formulate a common approach that could provide the spray parameters of airblast atomizers, various processes of liquid preparation, breakup, and secondary atomization have been included ...
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    Semianalytical Correlations for NOx, CO, and UHC Emissions 

    Source: Journal of Engineering for Gas Turbines and Power:;1993:;volume( 115 ):;issue: 003:;page 612
    Author(s): N. K. Rizk; H. C. Mongia
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: To meet the future goals of reduced emissions produced by gas turbine combustors, a better understanding of the process of formation of various pollutants is required. Both empirical and ...
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    A Semi-Analytical Emission Model for Diffusion Flame, Rich/Lean and Premixed Lean Combustors 

    Source: Journal of Engineering for Gas Turbines and Power:;1995:;volume( 117 ):;issue: 002:;page 290
    Author(s): N. K. Rizk; H. C. Mongia
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: To enhance gas turbine combustor performance and emissions characteristics, better design methods need to be developed. In the present investigation, an emission model that simulates a detailed ...
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    Multicomponent and High-Pressure Effects on Droplet Vaporization 

    Source: Journal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 002:;page 248
    Author(s): S. K. Aggarwal; H. C. Mongia
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper deals with the multicomponent nature of gas turbine fuels under high-pressure conditions. The study is motivated by the consideration that the droplet submodels that are currently ...
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    Three-Dimensional Gas Turbine Combustor Emissions Modeling 

    Source: Journal of Engineering for Gas Turbines and Power:;1993:;volume( 115 ):;issue: 003:;page 603
    Author(s): N. K. Rizk; H. C. Mongia
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An emission model that combines the analytical capabilities of three-dimensional combustor performance codes with mathematical expressions based on detailed chemical kinetic scheme is formulated. ...
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    A Computational Procedure for Diffuser-Combustor Flow Interaction Analysis 

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 001:;page 1
    Author(s): K. C. Karki; V. L. Oechsle; H. C. Mongia
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes a diffuser-combustor flow interaction analysis procedure for gas turbine combustion systems. The method is based on the solution of the Navier–Stokes equations in a generalized ...
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    Anchored CCD for Gas Turbine Combustor Design and Data Correlation 

    Source: Journal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 003:;page 535
    Author(s): A. M. Danis; D. L. Burrus; H. C. Mongia
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Correlations based on design database, combined with multidimensional computational combustion dynamics (CCD) models are used in the combustion design process. However, because of limitations in ...
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    A Semi-Analytical Finite Rate Two-Reactor Model for Gas Turbine Combustors 

    Source: Journal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 003:;page 495
    Author(s): J. H. Tonouchi; T. J. Held; H. C. Mongia
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A gas turbine combustor is modeled using a two-reactor, finite-rate mixing and chemistry gas particle approach. The first reactor, used to simulate combustion in the primary zone, permits ...
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