Connection between oscillatory propellant flow and HF combustion instability in rocket motors and theoretical treatment for describing flow in fuel pipe lines under transient or oscillatory conditions; method of characteristics is developed in way similar to that employed in 1-dimensional gas dynamic studies; diagrams constructed are position and state diagram; methods used for calculations.


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    Title :

    Method of calculating liquid flow fluctuations in rocket motor supply pipes


    Additional title:

    ARS J


    Contributors:
    Woods, W.A. (author)

    Published in:

    ARS Journal ; 31 , n 11


    Publication date :

    1961


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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