The simulation of the transition surfaces of air intakes of aviation gas turbine engine from a rectangular cross section at the entrance to a circular cross section at the outlet of the use of intermediate regular changeable cross sections with the use of computer technologies.


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    Titel :

    Modeling of cross sections and volumes of transitional surfaces of air intakes of aviation engines


    Beteiligte:


    Erscheinungsdatum :

    2002




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt




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