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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    Title :

    Adam II propulsion system and internal aerodynamics


    Additional title:

    SAE -- Paper


    Contributors:
    Havey, C.T. (author)

    Conference:

    SAE Meeting ; 1967 Propulsive wing



    Publication date :

    1967


    Size :

    9 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    ADAM II Propulsion System and Internal Aerodynamics

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