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    Combustor Stability and Emissions Research Using a Well-Stirred Reactor 

    Source: Journal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 001:;page 70
    Author(s): J. Zelina; D. R. Ballal
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The design and development of low-emissions, lean premixed aero or industrial gas turbine combustors is very challenging because it entails many compromises. To satisfy the projected CO and NOx ...
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    Weak Extinction Limits of Turbulent Flowing Mixtures 

    Source: Journal of Engineering for Gas Turbines and Power:;1979:;volume( 101 ):;issue: 003:;page 343
    Author(s): D. R. Ballal; A. H. Lefebvre
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An equation has been derived for predicting the weak extinction limits of stabilized flames supplied with turbulent, flowing mixtures of uniform composition. Experiments have been conducted to ...
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    Weak Extinction Limits of Turbulent Heterogeneous Fuel/Air Mixtures 

    Source: Journal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 002:;page 416
    Author(s): D. R. Ballal; A. H. Lefebvre
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental and theoretical studies are made of the factors governing the weak extinction limits of stabilized flames supplied with flowing mixtures of liquid fuel drops and air. The test ...
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    Studies of Lean Blowout in a Step Swirl Combustor 

    Source: Journal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 001:;page 72
    Author(s): M. D. Durbin; D. R. Ballal
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The design requirements of a modern gas turbine combustor are increasingly dictated by wide stability limits, short flame length, and uniform mixing. To achieve the best trade-off between these ...
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    Aerodynamics of Bluff-Body Stabilized Confined Turbulent Premixed Flames 

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 004:;page 783
    Author(s): J. C. Pan; M. D. Vangsness; D. R. Ballal
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed information on the influence of geometric and flow parameters on the structure and properties of recirculation zone in confined combusting flows is not available. In this paper, ...
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    Turbulent Combustion Properties Behind a Confined Conical Stabilizer 

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 001:;page 33
    Author(s): J. C. Pan; W. J. Schmoll; D. R. Ballal
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbulence properties were investigated in and around the recirculation zone produced by a 45 deg conical flame stabilizer of 25 percent blockage ratio confined in a pipe supplied with a ...
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    Fluid Dynamics of a Conical Flame Stabilizer 

    Source: Journal of Engineering for Gas Turbines and Power:;1989:;volume( 111 ):;issue: 001:;page 97
    Author(s): D. R. Ballal; T. H. Chen; W. J. Schmoll
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbulence measurements were performed on a 45 deg conical flame stabilizer with a 31 percent blockage ratio, mounted coaxially at the mouth of a circular pipe and supplied with a turbulent ...
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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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    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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