Experimental measurements of the wall static pressure on a yawed, tangent-ogive-cylinder model in supersonic flow are reported. The model tested was six calibers in length and had a one-caliber ogive section. Measurements were obtained at six longitudinal stations on the cylinder portion of the model for 15 deg increments in circumferential position at M = 2, 3, 4 and for angles of attack up to 10 deg. The data have been tabulated for convenience in evaluating inviscid flow field computations. These data should provide a good test for the coupling of subsonic, transonic, and supersonic inviscid flow computation techniques.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Measurements of wall static pressure on a yawed tangent-ogive-cylinder model


    Weitere Titelangaben:

    Messungen des statischen Wanddrucks an einem Spitzbogenzylindermodell bei Gierbewegungen


    Beteiligte:
    Sturek, W.B. (Autor:in) / Reba, J.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1976


    Format / Umfang :

    50 Seiten


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch




    Tangent-ogive nose cones

    Wing, L. D. | NTRS | 1976


    Temporal evolution of the flowfield over a pitching tangent ogive cylinder

    Zeiger, M / Rediniotis, O / Donnelley, M et al. | AIAA | 1995