Current trends in military combat aircraft are towards increased emphasis on multi-mission capability which requires engine sizing at flight conditions other than those of basic missions, such as for short takeoff, for acceleration/climb capability in combat, or for supersonic capability; assessment is made of magnitude of inlet drag associated with oversized engines; paper attempts to simplify engine cycle by examining flow matching of inlet with initial component of augmented turbofan engine -- fan; flow requirements are established for fan and effects on performance and stability explored without regard to turbine and exhaust nozzle matching needs. (12319)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Inlet and fan aerodynamics


    Weitere Titelangaben:

    SAE Paper


    Beteiligte:
    Taylor, R.P. (Autor:in)

    Kongress:

    SAE Meeting ; 1968 Inlets


    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Inlet and Fan Aerodynamics

    Taylor, Richard P. | SAE Technical Papers | 1968


    Methodologies for Turbofan Inlet Aerodynamics Prediction

    Godard, Benjamin / Ben Nasr, Nabil / Barrier, Raphaël et al. | AIAA | 2017



    Inlet ground vortex aerodynamics under headwind conditions

    Murphy, J.P. / MacManus, D.G. | Elsevier | 2010