Use of this analytical parameter, it is shown, highlights the distinction between cases which are dominated by trailing-edge separation, and those for which separation at the shock foot is dominant. Use of the analytical parameter and the distinction noted above greatly improves the correlation of separation data and the extrapolation of wind tunnel data to flight conditions.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    New considerations on scale extrapolation of wing pressure distributions affected by transonic shock-induced separations


    Contributors:

    Publication date :

    1983-03-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English