Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

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


    Contributors:

    Conference:

    52nd AIAA/SAE/ASEE Joint Propulsion Conference



    Publication date :

    2016-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    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 | European Patent Office | 2020

    Free access

    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