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    Gas Turbine Hot-Stage Parts in Aggressive Atmospheres 

    Source: Journal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;issue: 004:;page 540
    Author(s): S. Y. Lee; W. E. Young
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Westinghouse experience in burning heavy residual fuels in gas turbines dates back 25 years when such fuels were burned in a 2000 hp turbine powering a locomotive. In this paper we present ...
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    Laboratory Procedures for Evaluating High-Temperature Corrosion Resistance of Gas Turbine Alloys 

    Source: Journal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 003:;page 313
    Author(s): S. Y. Lee; S. M. DeCorso; W. E. Young
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: With an increasing interest in the burning of heavy fuels in gas turbines there is also concern with the precise determination of the corrosive effects which may arise from the use of these ...
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    Environmental Effects on the High-Temperature Corrosion of Superalloys in Present and Future Gas Turbines 

    Source: Journal of Engineering for Gas Turbines and Power:;1972:;volume( 094 ):;issue: 002:;page 149
    Author(s): S. Y. Lee; C. E. Hussey; W. E. Young
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Effects of temperature and contaminant levels on the high-temperature corrosion of superalloys used in gas turbines were investigated using pressurized passages which simulate the operating conditions ...
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    Investigation of Air Bearings for Small High-Performance Aircraft Gas Turbines 

    Source: Journal of Engineering for Gas Turbines and Power:;1972:;volume( 094 ):;issue: 004:;page 294
    Author(s): P. W. Curwen; W. E. Young; R. G. Furgurson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: High temperatures and rotative speeds of future U. S. Army aircraft propulsion systems will impose increasingly severe operating requirements on oil-lubricated engine bearings and associated seals. ...
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    Formation and Control of Oxides of Nitrogen Emissions From Gas Turbine Combustion Systems 

    Source: Journal of Engineering for Gas Turbines and Power:;1972:;volume( 094 ):;issue: 004:;page 271
    Author(s): P. P. Singh; M. J. Ambrose; W. E. Young
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Results of an investigation into the levels of oxides of nitrogen in Westinghouse gas turbine exhausts are presented. Various methods of controlling the amounts of these emissions were considered. ...
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    Evaluation of Additives for Prevention of High Temperature Corrosion of Superalloys in Gas Turbines 

    Source: Journal of Engineering for Gas Turbines and Power:;1973:;volume( 095 ):;issue: 004:;page 333
    Author(s): S. Y. Lee; G. Vermes; W. E. Young
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A number of commercially available chemical additives for utilization in modern high temperature gas turbines were evaluated for their corrosion and deposit inhibiting characteristics. The evaluation ...
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    Fuels for Advanced Power Generation Systems 

    Source: Journal of Engineering for Gas Turbines and Power:;1965:;volume( 087 ):;issue: 002:;page 125
    Author(s): S. Way; W. E. Young; I. S. Tuba; R. L. Chambers
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper discusses the relative merits of various fuels for magnetohydrodynamic power systems in which the MHD generator operates on combustion products and is coupled with a steam plant or ...
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    Experiments With MHD Power Generation 

    Source: Journal of Engineering for Gas Turbines and Power:;1961:;volume( 083 ):;issue: 004:;page 397
    Author(s): S. Way; S. M. DeCorso; R. L. Hundstad; G. A. Kemeny; W. Stewart; W. E. Young
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper is a report on the development of an experimental MHD electrical generator which derives its energy from the combustion of a liquid fuel and oxygen. The fuel burned is a number ...
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