Initial shocks of type that occur on airfoils at stream Mach numbers less than unity are shown to satisfy condition that local Mach number behind shock wave tends to approach unity; it is shown that mission of shock is essentially that of bringing local velocity back to local sonic value, that smaller shock is insufficient, and greater shock cannot be accommodated.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Condition on initial shock


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Theodorsen, T. (Autor:in)


    Erscheinungsdatum :

    1946


    Format / Umfang :

    7 pages


    Anmerkungen:

    Bibliography, Supp sheets


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    A condition on the initial shock

    Theodorsen, Theodore | TIBKAT | 1945


    A condition on the initial shock

    Theodorsen, Theodore | NTRS | 1946


    Initial flow model in shock tubes

    BRUN, R. / REBOH, R. | AIAA | 1977


    Initial management of shock in children

    Botte, A. / Leclerc, F. / SAMU | British Library Conference Proceedings | 2009


    MONITORING OF A SHOCK ABSORBER CONDITION

    GUIDOUX ANTOINE / SMITH JON / RAVEL JEAN-YVES et al. | Europäisches Patentamt | 2023

    Freier Zugriff