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    Titel :

    A Parametric Gas Turbine Modeling Approach for Assessing Transient Technologies in the Conceptual Design Phase


    Beteiligte:

    Kongress:

    51st AIAA/SAE/ASEE Joint Propulsion Conference



    Erscheinungsdatum :

    01.01.2015




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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