This investigation focuses on the development of multibody analytical models to predict the dynamic response, aeroelastic stability, and blade loading of a soft-inplane tiltrotor wind-tunnel model. Comprehensive rotorcraft-based multibody analyses enable modeling of the rotor system to a high level of detail such that complex mechanics and nonlinear effects associated with control system geometry and joint deadband may be considered. The influence of these and other nonlinear effects on the aeromechanical behavior of the tiltrotor model are examined. A parametric study of the design parameters which may have influence on the aeromechanics of the soft-inplane rotor system are also included in this investigation.


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    Title :

    Further Results of Soft-Inplane Tiltrotor Aeromechanics Investigation Using Two Multibody Analyses



    Conference:

    AHS International 60th Annual Forum ; 2004 ; Baltimore, MD, United States


    Publication date :

    2004-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Further Results of Soft-Inplane Tiltrotor Aeromechanics Investigation Using Two Multibody Analyses

    Masarati, P. / Quaranta, G. / Piatak, D. J. et al. | British Library Conference Proceedings | 2004



    Soft-Inplane Tiltrotor Aeromechanics Investigation Using Two Multibody Analyses

    Masarati, P. / Royal Aeronautical Society | British Library Conference Proceedings | 2005



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