Theory of small disturbances is applied to calculation of pressure distribution and drag of closed body of revolution traveling at supersonic speeds; it is shown that toward rear of body, shape of pressure distribution is similar to that for subsonic flow; for fineness ratios between 10 and 15, theoretical wave drag is of same order as probable values of frictional drag.


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    Titel :

    Flow over slender body of revolution at supersonic velocities


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Jones, R.T. (Autor:in) / Margolis, B. (Autor:in)


    Erscheinungsdatum :

    1946


    Format / Umfang :

    8 pages


    Anmerkungen:

    5 Supp sheets


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Flow over a slender body of revolution at supersonic velocities

    Jones, Robert T. / Margolies, Kenneth | TIBKAT | 1946


    Flow over a slender body of revolution at supersonic velocities

    Jones, Robert T / Margolis, Kenneth | NTRS | 1946




    Unsteady aerodynamic forces on slender body of revolution in supersonic flow

    Bond, R. / Packard, B.B. | Engineering Index Backfile | 1961