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:

    Erscheinungsdatum :

    08.07.1946


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    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




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