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    Discussion: “The Split Compressor Differential Gas Turbine Engine for Vehicle Propulsion” (Doyle, G. N., and Wilkinson, T. S., 1967, ASME J. Eng. Power, 89, pp. 49–59) 

    Source: Journal of Engineering for Gas Turbines and Power:;1967:;volume( 089 ):;issue: 001:;page 59
    Author(s): H. I. H. Saravanamuttoo
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Discussion: “Acceleration Performance Analysis of a Gas Turbine Destroyer Escort” (Bodnaruk, A., and Rubis, C. J., 1971, ASME J. Eng. Power, 93, pp. 49–55) 

    Source: Journal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 001:;page 55
    Author(s): H. I. H. Saravanamuttoo
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Closure to “Discussion of ‘Simulation of an Advanced Twin-Spool Industrial Gas Turbine’” (1992, J. Eng. Gas Turbines Power, 114, pp. 185–186) 

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002:;page 186
    Author(s): Ping Zhu; H. I. H. Saravanamuttoo
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Simulation of an Advanced Twin-Spool Industrial Gas Turbine 

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002:;page 180
    Author(s): Ping Zhu; H. I. H. Saravanamuttoo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A full-range mathematical model of the LM-1600 gas turbine has been developed, for future use in EHM studies. No data were available from the manufacturer other than sales brochures giving ...
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    Predicting Gas Turbine Performance Degradation Due to Compressor Fouling Using Computer Simulation Techniques 

    Source: Journal of Engineering for Gas Turbines and Power:;1989:;volume( 111 ):;issue: 002:;page 343
    Author(s): G. F. Aker; H. I. H. Saravanamuttoo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: As part of an ongoing investigation into the effects of compressor fouling on gas turbine performance, the stage stacking technique was used in conjunction with generalized turbine characteristics ...
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    Simulating Indirect Thrust Measurement Methods for High-Bypass Turbofans 

    Source: Journal of Engineering for Gas Turbines and Power:;1995:;volume( 117 ):;issue: 001:;page 38
    Author(s): J. D. Stevenson; H. I. H. Saravanamuttoo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: As yet, there is no known reliable method for directly measuring the thrust of a turbofan in flight. Manufacturers of civil turbofans use various indirect thrust measurements to indicate ...
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    Experimental Investigation of Methods for Improving the Dynamic Response of a Twin-Spool Turbojet Engine 

    Source: Journal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 004:;page 418
    Author(s): A. J. Fawke; H. I. H. Saravanamuttoo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes experimental tests carried out on a twin-spool turbojet to confirm earlier simulator predictions of methods of improving the dynamic response. The engine was controlled by ...
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    A Proposed Method for Assessing the Susceptibility of Axial Compressors to Fouling 

    Source: Journal of Engineering for Gas Turbines and Power:;1991:;volume( 113 ):;issue: 004:;page 595
    Author(s): F. Seddigh; H. I. H. Saravanamuttoo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Although the overall effect of compressor fouling on engine performance has been recognized for many years, remarkably little has been published on the quantifiable effects. Mathematical modeling ...
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    Thermodynamic Models for Pipeline Gas Turbine Diagnostics 

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 004:;page 875
    Author(s): H. I. H. Saravanamuttoo; B. D. MacIsaac
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Thermodynamic models suitable for use as diagnostic tools for pipeline gas turbines have been developed. A basic requirement was the prediction of the performance of gas turbines subject to ...
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    Health Monitoring of Variable Geometry Gas Turbines for the Canadian Navy 

    Source: Journal of Engineering for Gas Turbines and Power:;1989:;volume( 111 ):;issue: 002:;page 244
    Author(s): D. E. Muir; H. I. H. Saravanamuttoo; D. J. Marshall
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The Canadian Department of National Defence has identified a need for improved Engine Health Monitoring procedures for the new Canadian Patrol Frigate (CPF). The CPF propulsion system includes ...
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