Basic use of drogue is to augment aerodynamic drag and moments (both static and dynamic) of primary body; drag measurements for spherical and conical drogues behind various forebody shapes were made at supersonic speeds by free-flight testing technique; major variables investigated were ratio of drogue diameter to forebody diameter and ratio of towline length to forebody diameter; investigations of various forebody-drogue configurations were conducted at Mach 4; effects of Mach number (0.7 greater than M greater than 4) were carried out only on Apollo-like forebody with spherical drogue. (17465)


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    Titel :

    Forebody effects on drogue drag in supersonic flow


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Dayman, Jr., B. (Autor:in) / Kurtz, D.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Forebody effects on drogue drag in supersonic flow.

    DAYMAN, B. / KURTZ, D. W. | AIAA | 1968


    Forebody effects on drogue drag in supersonic flow.

    Dayman, B., Jr. / Kurtz, D. W. | NTRS | 1968


    Forebody effects on drogue drag in supersonic flow.

    Dayman, B., Jr. / Kurtz, D. W. | NTRS | 1968


    Forebody effects on drogue drag in supersonic flow

    DAYMAN, JR., B. / KURTZ, D. | AIAA | 1968


    Numerical Assessment of Heterogeneous Plasma Discharge Effects on Supersonic Forebody Drag

    Wilkerson, Jordan / Van Wie, David / Cybyk, Bohdan | AIAA | 2003