The vortical flow on the leeward side of a delta-wing model has been visualized at several different tunnel conditions in the NASA Langley 0.3-Meter Transonic Cryogenic Tunnel using a vapor-screen flow-visualization technique. Vapor-screen photographs of the subject flow field are presented and interpreted relative to phenomenological implications. Results indicate that the use of nitrogen fog in conjunction with the vapor-screen technique is feasibile.


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    Titel :

    Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel


    Beteiligte:
    Selby, G. V. (Autor:in)

    Erscheinungsdatum :

    1986-05-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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