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    Discussion: “Multiple Jet Correlations for Gas Turbine Engine Combustor Design” (Cox, Jr., G. B., 1976, ASME J. Eng. Power, 98, pp. 265–272) 

    Source: Journal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;issue: 002:;page 272
    Author(s): J. D. Holdeman
    Publisher: The American Society of Mechanical Engineers (ASME)
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    The Initiation, Development, and Decay of the Secondary Flow in a Bounded Jet 

    Source: Journal of Fluids Engineering:;1975:;volume( 097 ):;issue: 003:;page 342
    Author(s): J. D. Holdeman; J. F. Foss
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The secondary flow in a low aspect ratio incompressible turbulent bounded jet is described in terms of a near, middle, and far field in which the secondary motion is initiated, developed, and ...
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    Spreadsheet Calculations for Jets in Crossflow From Single and Opposed Rows With Alternating Hole Sizes 

    Source: Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 006:;page 64502
    Author(s): J. D. Holdeman; J. R. Clisset; J. P. Moder
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The primary purpose of this study was to show the expected results for cases of single and opposed rows of jets from alternating large and small round holes. Previous publications demonstrated ...
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    Mixing of Multiple Jets With a Confined Subsonic Crossflow: Part II—Opposed Rows of Orifices in Rectangular Ducts 

    Source: Journal of Engineering for Gas Turbines and Power:;1999:;volume( 121 ):;issue: 003:;page 551
    Author(s): J. D. Holdeman; D. S. Liscinsky; D. B. Bain
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper summarizes experimental and computational results on the mixing of opposed rows of jets with a confined subsonic crossflow in rectangular ducts. The studies from which these results ...
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    CFD Analysis of Jet Mixing in Low NOx Flametube Combustors 

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002:;page 416
    Author(s): M. V. Talpallikar; M. C. Lai; J. D. Holdeman; C. E. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The Rich-burn/Quick-mix/Lean-burn (RQL) combustor has been identified as a potential gas turbine combustor concept to reduce NOx emissions in High Speed Civil Transport (HSCT) aircraft. To demonstrate ...
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    Mixing of Multiple Jets With a Confined Subsonic Crossflow: Part I—Cylindrical Duct 

    Source: Journal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 004:;page 852
    Author(s): J. D. Holdeman; D. S. Liscinsky; V. L. Oechsle; G. S. Samuelsen; C. E. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper summarizes NASA-supported experimental and computational results on the mixing of a row of jets with a confined subsonic crossflow in a cylindrical duct. The studies from which these ...
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