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    The Meaning of Activation Energy and Reaction Order in Autoaccelerating Systems 

    Source: Journal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 003:;page 468
    Author(s): J. S. Ervin; S. P. Heneghan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Global reaction mechanisms and rate constants are commonly used in computational fluid dynamics models that incorporate chemical reactions to study aviation fuel thermal and oxidative thermal ...
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    Lean Blowout in a Research Combustor at Simulated Low Pressures 

    Source: Journal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 004:;page 773
    Author(s): G. J. Sturgess; S. P. Heneghan; A. L. Lesmerises; M. D. Vangsness; D. R. Ballal
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A propane-fueled research combustor has been designed to represent the essential features of primary zones of combustors for aircraft gas turbine engines in an investigation of lean blowouts. ...
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    Surface Effects on Deposits From Jet Fuels 

    Source: Journal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 002:;page 278
    Author(s): J. S. Ervin; S. P. Heneghan; C. R. Martel; T. F. Williams
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Flow experiments in a single-pass heat exchanger using JP-8 and certain additives were initiated under controlled conditions to explore the effects of a metal surface on deposition. The experimental ...
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    JP-8+100: The Development of High-Thermal-Stability Jet Fuel 

    Source: Journal of Energy Resources Technology:;1996:;volume( 118 ):;issue: 003:;page 170
    Author(s): S. P. Heneghan; W. E. Harrison; S. Zabarnick; D. R. Ballal
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Jet fuel requirements have evolved over the years as a balance of the demands placed by advanced aircraft performance (technological need), fuel cost (economic factors), and fuel availability ...
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    Design and Development of a Research Combustor for Lean Blow-Out Studies 

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 001:;page 13
    Author(s): G. J. Sturgess; A. L. Lesmerises; S. P. Heneghan; D. R. Ballal; D. G. Sloan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In a modern aircraft gas turbine combustor, the phenomenon of lean blow-out (LBO) is of major concern. To understand the physical processes involved in LBO, a research combustor was designed ...
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    Isothermal Flow Fields in a Research Combustor for Lean Blowout Studies 

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002:;page 435
    Author(s): G. J. Sturgess; S. P. Heneghan; A. L. Lesmerises; M. D. Vangsness; D. R. Ballal
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A propane-fueled research combustor has been designed and developed to investigate lean blowouts in a simulated primary zone of the combustors for aircraft gas turbine engines. To understand the ...
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    The Effects of Dissolved Oxygen Concentration, Fractional Oxygen Consumption, and Additives on JP-8 Thermal Stability 

    Source: Journal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 004:;page 822
    Author(s): J. S. Ervin; T. F. Williams; S. P. Heneghan; S. Zabarnick
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Since dissolved oxygen participates in fuel deposit formation, knowledge of the effects of dissolved oxygen concentration on fuel thermal stability is critical for fuel system design. In this ...
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    Effects of Oxygen and Additives on the Thermal Stability of Jet Fuels 

    Source: Journal of Engineering for Gas Turbines and Power:;1995:;volume( 117 ):;issue: 001:;page 120
    Author(s): S. P. Heneghan; C. R. Martel; T. F. Williams; D. R. Ballal
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A previously developed flowing single-pass heat-exchanger test rig (Phoenix rig) has been used to evaluate the effectiveness of various additives and the kinetic mechanism of both deposit formation ...
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    Studies of Jet Fuel Thermal Stability in a Flowing System 

    Source: Journal of Engineering for Gas Turbines and Power:;1993:;volume( 115 ):;issue: 003:;page 480
    Author(s): S. P. Heneghan; C. R. Martel; T. F. Williams; D. R. Ballal
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A flowing, single-pass heat exchanger test rig, with a fuel capacity of 189 liters, has been developed to evaluate jet fuel thermal stability. This “Phoenix Rig” is capable of supplying jet ...
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    Effects of Back-Pressure in a Lean Blowout Research Combustor 

    Source: Journal of Engineering for Gas Turbines and Power:;1993:;volume( 115 ):;issue: 003:;page 486
    Author(s): G. J. Sturgess; S. P. Heneghan; A. L. Lesmerises; D. Shouse; M. D. Vangsness; D. R. Ballal
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental information is presented on the effects of back-pressure on flame-holding in a gaseous fuel research combustor. Data for wall temperatures and static pressures are used to infer ...
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