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


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    Titel :

    Flow over a slender body of revolution at supersonic velocities


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


    Erscheinungsdatum :

    01.02.1976


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Flow over slender body of revolution at supersonic velocities

    Jones, R.T. / Margolis, B. | Engineering Index Backfile | 1946


    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