Transonic nonsteady flows are of large practical interest. Aeroelastic instability prediction, control figured vehicle techniques or rotary wings in forward flight are some examples justifying the effort undertaken to improve knowledge of these problems is described. The numerical solution of these problems under the potential flow hypothesis is described. The use of an alternating direction implicit scheme allows the efficient resolution of the two dimensional transonic small perturbations equation.


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    Title :

    Transonic small disturbances equation applied to the solution of two-dimensional nonsteady flows


    Contributors:
    Couston, M. (author) / Angelini, J. J. (author) / Mulak, P. (author)

    Publication date :

    1980-04-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :