Propellant sloshing may be caused by bending of space vehicle that exhibits low structural frequencies; forces and moments exerted by oscillating propellant on tank are determined due to forced bending excitation for liquid in circular, cylindrical, ring sector tank with free fluid surface; as is expected, force and moment of liquid increase sharply at resonant frequencies of propellant; maximum dynamic effects occur when free fluid surface is located in vicinity of point of maximum bending displacement.


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    Title :

    Theory of liquid sloshing in compartmented cylindrical tanks due to bending excitation


    Additional title:

    AIAA J


    Contributors:
    Bauer, H.F. (author)

    Published in:

    AIAA Journal ; 1 , n 7


    Publication date :

    1963


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English