An attempt is made to indicate and briefly discuss only the most significant achievements of the research. The most successful contribution from the contract was the code for two dimensional analysis of airfoils in transonic flow.


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    Title :

    Numerical design of shockless airfoils


    Contributors:

    Publication date :

    1979-02-28


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Shockless transonic airfoils

    TRUITT, R. | AIAA | 1970



    Experimental evaluation of shockless supercritical airfoils in cascade

    Boldman, D. R. / Buggele, A. E. / Shaw, L. M. | NTRS | 1983


    Experimental evaluation of shockless supercritical airfoils in cascade

    BOLDMAN, D. / BUGGELE, A. / SHAW, L. | AIAA | 1983


    Experimental evaluation of shockless supercritical airfoils in cascade

    Boldman, D. R. / Buggele, A. E. / Shaw, L. M. | NTRS | 1983