Typical ejector wing, remote fan-in-wing, remote lift/cruise fan, and lift plus lift/cruise propulsion concepts are parametrically studied on the basis of airplane weights (gross, empty, and propulsion) for three types of airplanes, a Carrier-Onboard Delivery/Search and Rescue airplane for the U.S. Navy, a military utility transport, and a business jet. None of the four systems led to airplanes substantially lighter than the others, and therefore no best system is selected. (Author)


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    Titel :

    Conceptual Study of Four Subsonic VTOL Propulsion Systems


    Beteiligte:
    W. C. Strack (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    33 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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