The Ducted Propulsor is proposed as a means of quiet propulsion. In order to demonstrate that very low levels can be realistically achieved, a unit has been built based on a conventional 285 h.p. aircraft reciprocating engine.The problems associated with the design of such a power plant, which include keeping the cost and weight of a production unit in perspective, are discussed along with the chosen solution. The test results will be published later.


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    Titel :

    A Ducted Propulsor Demonstrator


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Davis, D.G.M. (Autor:in)

    Kongress:

    National Business Aircraft Meeting and Engineering Display ; 1976



    Erscheinungsdatum :

    01.02.1976




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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