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    Titel :

    Design of an Additive Manufactured Compressor Vane with Multi-Hole Pressure Probes for the Application in a Twin-Spool Turbofan Engine


    Beteiligte:
    Kern, Felix (Autor:in) / Bindl, Stefan (Autor:in) / Strasser, Martin (Autor:in) / Niehuis, Reinhard (Autor:in)

    Kongress:

    52nd AIAA/SAE/ASEE Joint Propulsion Conference



    Erscheinungsdatum :

    01.01.2016




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    DESIGN OF AN ADDITIVE MANUFACTURED COMPRESSOR VANE WITH MULTI-HOLE PRESSURE PROBES FOR THE APPLICATION IN A TWIN-SPOOL TURBOFAN ENGINE (AIAA 2016-4508)

    Kern, Felix / Bindl, Stefan / Strasser, Martin et al. | British Library Conference Proceedings | 2016



    Effect of Pressure Recovery on Triple Spool Turbofan Engine Performance

    Khalil, Essam E. / AbdelGhany, Eslam / Fouad, Mahmoud A. et al. | AIAA | 2013


    SPLIT COMPRESSOR SYSTEM ON MULTI-SPOOL ENGINE

    PLANTE GHISLAIN / MORGAN KEITH / COUTURE-GAGNON VINCENT | Europäisches Patentamt | 2020

    Freier Zugriff

    ACTIVE STABILIZATION OF THE COMPRESSION SYSTEM IN A TWIN-SPOOL TURBOFAN ENGINE AT INLET DISTORTIONS

    Scheidler, S. G. / Fottner, L. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2003