The preliminary design and installation of high bypass, geared turbofan engine with a composite nacelle forming the propulsion system for a short haul passenger aircraft are described. The technology required for externally blown flap aircraft with under the wing (UTW) propulsion system installations for introduction into passenger service in the mid 1980's is included. The design, fabrication, and testing of this UTW experimental engine containing the required technology items for low noise, fuel economy, with composite structure for reduced weight and digital engine control are provided.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Quiet Clean Short-haul Experimental Engine (QCSEE) preliminary under the wing flight propulsion system analysis report


    Contributors:

    Publication date :

    1976-02-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English