Stability of liquid propellant missiles and spacecraft, controlled by autopilot system, is affected by propellant motions in tanks; response of propellant to sinusoidal forced motions, as translational, rotational, and bending oscillations of tank walls, is treated; velocity potential, free fluid surface displacement, pressure and velocity distribution in tanks, fluid forces, and moments were determined for small oscillations.


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    Titel :

    Theory of fluid oscillations in circular cylindrical ring tank partially filled with liquid


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Bauer, H.F. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    124 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :