Abstract A functional IDEF0-model of conceptual design of an aircraft gas turbine engine was developed. By an example of selecting a structural design of two-rotor gas turbine engine, we present the structured analysis of the engine and describe the operation of the genetic algorithm.


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    Titel :

    Synthesis of basic structural design of aircraft GTE based on genetic algorithms


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    2015-04-01


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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