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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    Title :

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


    Contributors:

    Published in:

    Publication date :

    2015-04-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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