These lectures address numerous engine airframe integration aspects relating to rotor wing aircraft. Various areas of engine airframe integration, including the impact of advanced engine design variables to specific propulsion subsystems, i.e. engine air inlets, are discussed. Other propulsion system integration aspects such as engine/rotor/drive system torsional stability and transient response are also addressed.


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    Airframe/Engine Integration

    A. Ferri | NTIS | 1972


    Engine-airframe integration

    Nicholson, L.F. | Engineering Index Backfile | 1957


    Airframe engine integration

    NATO, Advisory Group for Aerospace Research and Development | TIBKAT | 1972


    STOVL engine/airframe integration

    BUCKNELL, R. L. | AIAA | 1989


    ROTORCRAFT AND CONNECTING STRUCTURE FOR ARM AND AIRFRAME OF ROTORCRAFT

    PENG BIN / XIAO DINGFENG | Europäisches Patentamt | 2019

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