The element and subcomponent testing conducted to verify the under the wing composite nacelle design is reported. This composite nacelle consists of an inlet, outer cowl doors, inner cowl doors, and a variable fan nozzle. The element tests provided the mechanical properties used in the nacelle design. The subcomponent tests verified that the critical panel and joint areas of the nacelle had adequate structural integrity.


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    Title :

    Quiet Clean Short-Haul Experimental Engine (QCSEE) under-the-Wing (UTW) Composite Nacelle Subsystem Test Report


    Contributors:

    Publication date :

    1977


    Size :

    83 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English