Adam II (Air Deflection and Modulation) propulsion system as applied to LTV propulsive wing airplane configurations which house all, or part, of their propulsion system within wing surface; briefly mentioned are original ADAM I configuration and its subsequent development to present ADAM II, together with discussion of characteristics currently used for each component such as fan turbine set, gas generator, hot gas ducting, wing mounted turbofans, and mechanical cross shafting; ADAM II concept is applicable to full spectrum of subsonic aircraft, and propulsion system uses present day state-of-art technology which makes feasibility of its development quite real.


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    Titel :

    Adam II propulsion system and internal aerodynamics


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Havey, C.T. (Autor:in)

    Kongress:

    SAE Meeting ; 1967 Propulsive wing



    Erscheinungsdatum :

    1967


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    ADAM II Propulsion System and Internal Aerodynamics

    Havey, C. Todd | SAE Technical Papers | 1967


    Aerodynamics of propulsion

    Küchemann, Dietrich ;Weber, Johanna | SLUB | 1953


    Aerodynamics of propulsion

    Küchemann, Dietrich / Weber, Johanna | GWLB - Gottfried Wilhelm Leibniz Bibliothek | 1953


    Aerodynamics of propulsion

    Küchemann, Dietrich / Weber, Johanna | TIBKAT | 1953