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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    NASA -- Tech Note


    Contributors:
    Bauer, H.F. (author)


    Publication date :

    1960


    Size :

    124 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English