A real gas laminar boundary-layer separation methodology has been developed to predict Space Shuttle Orbiter control surface effectiveness during atmospheric entry. The methodology is based on the Lees-Klineberg moment integral theory. A real gas laminar boundary-layer model, having a binary atomic diffusion of frozen gas composition, is assumed. A brief discussion of theory and sample results are presented herein. A set of boundary-layer profile parameters which are required for this theory is given in the full paper. (Jensen)


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    Title :

    Real gas laminar boundary-layer separation prediction methodology


    Additional title:

    Methode der Vorhersage der Stroemungsabtrennung bei laminarer Grenzschichtstroemung


    Contributors:
    Ikawa, H. (author)

    Published in:

    AIAA Journal ; 17 , 11 ; 1157-1158


    Publication date :

    1979


    Size :

    2 Seiten, 4 Bilder, 4 Quellen



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English