The aerodynamic development of the engine nacelle for the Boeing 767 airplane is described from configuration development model tests to FAA certification flight tests. Details of the inlet, nozzles and thrust reverser development in conjunction with the engine are discussed.


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    Title :

    Aerodynamic Development of the Engine Nacelle Combination for the Boeing 767 Airplane


    Additional title:

    Sae Technical Papers


    Contributors:
    Neal, Brian (author)

    Conference:

    International Air Transportation Meeting ; 1980



    Publication date :

    1980-04-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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