The fuselage torsion mode of a CT4 aircraft has been examined using an impulsive testing technique. The mode shape and natural frequency are presented. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Fuselage Torsion of a CT4 Aircraft


    Contributors:
    P. M. Cox (author) / A. Goldman (author)

    Publication date :

    1983


    Size :

    25 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Aircraft fuselage section, aircraft fuselage and aircraft

    LINDE PETER / MATTHIAS HEGENBART | European Patent Office | 2023

    Free access

    AIRCRAFT STABILIZER LEADING EDGE INTEGRATION WITH TORSION BOX AND FUSELAGE

    ARANA HIDALGO ALBERTO / MARTINO GONZÁLEZ ESTEBAN / VÁZQUEZ CASTRO JESÚS JAVIER et al. | European Patent Office | 2019

    Free access

    AIRCRAFT STABILIZER LEADING EDGE INTEGRATION WITH TORSION BOX AND FUSELAGE

    ARANA HIDALGO ALBERTO / MARTINO GONZÁLEZ ESTEBAN / VÁZQUEZ CASTRO JESÚS JAVIER et al. | European Patent Office | 2018

    Free access

    Aircraft fuselage

    VAN BAVEL LUC / DERMAN MICHAEL | European Patent Office | 2022

    Free access

    FUSELAGE SECTION OF AN AIRCRAFT, AIRCRAFT FUSELAGE, AND AIRCRAFT

    LINDE PETER / HEGENBART MATTHIAS | European Patent Office | 2023

    Free access