The analytical development of unsteady supersonic aerodynamic influence coefficients for isolated and nearly parallel interfering coplanar and noncoplanar wings is described. Numerical formulations based on triangular discretizations of wings and diaphragms are handled in a kinematically consistent manner. Examples of isolated wing cases are compared with respect to aerodynamic influence coefficients and flutter boundaries. Aerodynamic influence coefficients for interfering wings are compared where corresponding results are available.


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    Title :

    Development and applications of supersonic unsteady consistent aerodynamics for interfering parallel wings


    Contributors:
    Appa, K. (author) / Smith, G. C. C. (author)

    Publication date :

    1973-03-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :