Aspects of confluence of 2 streams over region of afterbodies are explained; analysis can be reduced to 3 fundamental problems, development of isobaric mixing zone, separation and reattachment of flow; theoretical results achieved by ONERA (Office Nat d'Etudes et de Recherches Aeronautiques) are presented; several examples of application in regions of hypersonic and supersonic flow.


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    Title :

    Investigation of flow over afterbodies of aircraft or rockets


    Additional title:

    Untersuchungen ueber die Stroemung am Heck von Flugzeugen oder Raketen


    Contributors:

    Published in:

    Publication date :

    1962


    Size :

    13 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German


    Keywords :




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