The objective of this research is to develop optimization procedures to provide design trends in high speed prop-rotors. The necessary disciplinary couplings are all considered within a closed loop optimization process. The procedures involve the consideration of blade aeroelastic, aerodynamic performance, structural and dynamic design requirements. Further, since the design involves consideration of several different objectives, multiobjective function formulation techniques are developed.


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    Title :

    Optimum Design of High Speed Prop-Rotors


    Contributors:

    Publication date :

    1992-10-12


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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