Coupling of aeromechanics analysis with vehicle sizing is demonstrated with the CAMRAD II aeromechanics code and NDARC sizing code. The example is optimization of cruise tip speed with rotor/wing interference for the Large Civil Tiltrotor (LCTR2) concept design. Free-wake models were used for both rotors and the wing. This report is part of a NASA effort to develop an integrated analytical capability combining rotorcraft aeromechanics, structures, propulsion, mission analysis, and vehicle sizing. The present paper extends previous efforts by including rotor/wing interference explicitly in the rotor performance optimization and implicitly in the sizing.


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    Titel :

    Integration of Rotor Aerodynamic Optimization with the Conceptual Design of a Large Civil Tiltrotor


    Beteiligte:

    Kongress:

    AHS Aeromechanics Specialists Conference 2010 ; 2010 ; San Francisco, CA, United States


    Erscheinungsdatum :

    20.01.2010


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch