The quasianalytical approach is applied to the 3-D full potential equation to compute wing aerodynamic sensitivity coefficients in the transonic regime. Symbolic manipulation is used to reduce the effort associated with obtaining the sensitivity equations, and the large sensitivity system is solved using 'state of the art' routines. The quasianalytical approach is believed to be reasonably accurate and computationally efficient for 3-D problems.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Determination of aerodynamic sensitivity coefficients for wings in transonic flow


    Contributors:

    Publication date :

    1992-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :