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    Components Map Generation of Gas Turbine Engine Using Genetic Algorithms and Engine Performance Deck Data 

    Source: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 002:;page 312
    Author(s): Changduk Kong; Jayoung Ki
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In order to estimate the gas turbine engine performance precisely, the component maps containing their own performance characteristics should be used. Because the components map is an engine ...
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    Fuzzy Approaches for Searching Optimal Component Matching Point in Gas Turbine Performance Simulation 

    Source: Journal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 004:;page 741
    Author(s): Changduk Kong; Jayoung Ki; Myoungcheol Kang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In performance simulation of gas turbine, some iteration processes for searching the operating point, which should be matched through gas path components, would be needed. Therefore if the engine ...
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    Component Map Generation of a Gas Turbine Using Genetic Algorithms 

    Source: Journal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 001:;page 92
    Author(s): Changduk Kong; Seonghee Kho; Jayoung Ki
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In order to estimate the precise performance of the existing gas turbine engine, the component maps with more realistic performance characteristics are needed. Because the component maps are the ...
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    A Study on Transient Performance Characteristics of the Canard Rotor Wing Type Unmanned Aerial Vehicle Propulsion System During Flight Mode Transition 

    Source: Journal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 003:;page 573
    Author(s): Changduk Kong; Jongha Park; Myoungcheol Kang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A propulsion system of the CRW (Canard rotor wing) type UAV (unmanned aerial vehicle) was composed of the turbojet engine, exhaust nozzles (including some tip jet nozzles and a main nozzle), ...
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    Steady-State and Transient Performance Modeling of Smart UAV Propulsion System Using SIMULINK 

    Source: Journal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 003:;page 31702
    Author(s): Jayoung Ki; Changduk Kong; Changho Lee; Seonghee Kho
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Because an aircraft gas turbine operates under various flight conditions that change with altitude, flight velocity, and ambient temperature, the performance estimation that considers the flight ...
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