The equations of motion for the longitudinal dynamics of a tilting prop/rotor aircraft are developed. The analysis represents an extension of the equations of motion. The effects of the longitudinal degrees of freedom of the body (pitch, heave and horizontal velocity) are included. The results of body freedom can be added to the equations of motion for the flexible wing propeller combination. (Author)


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    Title :

    The Longitudinal Equations of Motion of a Tilt Prop/Rotor Aircraft Including the Effects of Wing and Prop/Rotor Blade Flexibility


    Contributors:

    Publication date :

    1976


    Size :

    63 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







    TILT PROP AIRCRAFT

    CHO JUN HO / LEE MYEONG KYU / CHOI SEONG WOOK | European Patent Office | 2024

    Free access

    Tilt Prop aircraft

    CHO JUN HO / LEE MYEONG KYU / CHOI SEONG WOOK | European Patent Office | 2024

    Free access