The dynamics of a highly maneuverable subsonic aircraft during multiple roll around the length axis were investigated with a 6 deg of freedom computer program. The nonlinear dependencies on the aerodynamic forces and moments are taken into account. The effect of the dynamic derivation of lateral motion on the overall motion is shown. The relationship between the position of the overall rotation vector and the velocity vector is represented.


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    Title :

    Investigation of Flight Dynamics During Roll Untersuchung der Flugdynamik Beim Rollen


    Contributors:
    H. D. Finck (author) / G. Sachs (author)

    Publication date :

    1976


    Size :

    58 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English