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.
Method of calculating liquid flow fluctuations in rocket motor supply pipes
ARS J
ARS Journal ; 31 , n 11
1961
8 pages
Article (Journal)
English
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