A study was conducted to establish a coupled rotor/propulsion analysis that would be applicable to a wide range of rotorcraft systems. The effort included the following tasks: (1) development of a model structure suitable for simulating a wide range of rotorcraft configurations; (2) defined a methodology for parameterizing the model structure to represent a particular rotorcraft; (3) constructing a nonlinear coupled rotor/propulsion model as a test case to use in analyzing coupled system dynamics; and (4) an attempt to develop a mostly linear coupled model derived from the complete nonlinear simulations. Documentation of the computer models developed is presented.


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    Titel :

    Development of a rotorcraft. Propulsion dynamics interface analysis, volume 2


    Beteiligte:
    Hull, R. (Autor:in)

    Erscheinungsdatum :

    1982-08-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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