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    The Transfer Number of Hydrocarbon Liquids 

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002:;page 346
    Author(s): J. Odgers; D. Kretschmer
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The transfer number (B) assumes considerable importance in the evaporation and diffusion of fuels prior to their combustion. Quite often the transfer number is assumed to be a constant for a ...
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    The Prediction of Laminar Flame Speeds for Weak Mixtures 

    Source: Journal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 003:;page 566
    Author(s): D. Kretschmer; J. Odgers
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In a recent publication [3], the authors tentatively explored the prediction of propane flame speeds using the calculated burned gas temperature (Tb ) and the predicted flame extinction temperature ...
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    Modeling of Gas Turbine Combustors—A Convenient Reaction Rate Equation 

    Source: Journal of Engineering for Gas Turbines and Power:;1972:;volume( 094 ):;issue: 003:;page 173
    Author(s): D. Kretschmer; J. Odgers
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In order to model a practical combustion system successfully, it is necessary to develop one or more reaction rate equations which will describe performance over a wide range of conditions. ...
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    The Pulsed Thermocouple for Gas Turbine Application 

    Source: Journal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 001:;page 1
    Author(s): D. Kretschmer; J. Odgers; A. F. Schlader
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A mechanically pulsed suction thermocouple has been developed. The gas to be measured is sucked through a sonic orifice, thus eliminating the influence of the velocity inside the combustor. The ...
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    Weak Limits of Premixed Gases 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 001:;page 10
    Author(s): J. Odgers; D. Kretschmer; J. Halpin
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental values of weak and rich limits, for a wide range of fuel-oxygen-inerts mixtures (H2 , CO, CH4 , C3 H8 , O2 , Ar, He, N2 , CO2 ), are presented for a number of tube diameters. ...
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    The Experimental Behavior of Premixed Flames in Tubes: The Effects of Diluent Gases 

    Source: Journal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 002:;page 422
    Author(s): J. Odgers; I. White; D. Kretschmer
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: One of the problems facing gas turbine users is the proliferation of gaseous fuels which may be available. These are so many that a comprehensive rig/engine study would be far too costly to ...
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    The Combustion of Droplets Within Gas Turbine Combustors: Some Recent Observations on Combustion Efficiency 

    Source: Journal of Engineering for Gas Turbines and Power:;1993:;volume( 115 ):;issue: 003:;page 522
    Author(s): J. Odgers; G. F. Pearce; D. Kretschmer
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: For many years investigators studying the combustion behavior within gas turbines have presumed droplet size to play a very important role in defining combustion efficiency. Recently a very large ...
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    Fuel Property Effects Upon Exhaust Smoke and the Weak Extinction Characteristics of the Pratt & Whitney PT6A-65 Engine 

    Source: Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 001:;page 175
    Author(s): P. Sampath; D. Kretschmer; J. Odgers; M. Gratton
    Publisher: The American Society of Mechanical Engineers (ASME)
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