It is assumed that pure antisymmetric vibrations can exist, involving fuselage torsion but excluding fuselage bending; with this assumption, eigenvalue equations for anti-symmetric vibrations of complete aircraft are derived in very general form.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Anti-symmetric vibrations of aircraft


    Additional title:

    Aeronautical Quarterly


    Contributors:

    Published in:

    Publication date :

    1951


    Size :

    16 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Vibrations in Aircraft

    Manley, R.G. | Emerald Group Publishing | 1944


    Vibrations in aircraft

    Manley, R.G. | Engineering Index Backfile | 1944


    Vibrations in Aircraft

    Manley, R.G. | Emerald Group Publishing | 1944


    Vibrations in Aircraft

    Manley, R.G. | Emerald Group Publishing | 1944


    Vibrations in Aircraft

    Manley, R.G. | Emerald Group Publishing | 1944