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Digital Distributed Parameter Model for Analysis of Unsteady Flow in Liquid-Filled LinesA distributed parameter model for computing unsteady flow conditions in liquid systems is presented. The model is adapted for use in conjunction with a digital computer. The analytical method employed is essentially a solution synthesized from the effects of incremental step pressure pulses. The pressure pulses are generated because of incremental flow-rate changes that originate in a fluid system from a variety of sources, including the mechanical motion of the system structure. The pressure pulses propagate throughout the system at sonic velocity and are partially transmitted and reflected at each discontinuity. The velocity change caused by each pressure pulse is obtained from the relation for the characteristic acoustic impedance. Pressure and velocity time histories at any point in the system are obtained by a timewise summation of the contributions of the incremental pressure pulses passing that point. The analysis is presented in a form general enough to be applied to a variety of liquid-filled fluid systems. To illustrate the application of the method to a specific system, the response of a long, straight propellant line to a sinusoidal inlet flow and pressure perturbation is computed. Both a constant-cross-section line and a tapered line are analyzed in the example.
Document ID
19650014113
Acquisition Source
Headquarters
Document Type
Other - NASA Technical Note (TN)
Authors
Wood, Don J.
(Kentucky Univ. Lexington, KY, United States)
Dorsch, Robert G.
(NASA Lewis Research Center Cleveland, OH, United States)
Lightner, Charlene
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1965
Subject Category
Fluid Mechanics
Report/Patent Number
E-2587
NASA-TN-D-2812
Report Number: E-2587
Report Number: NASA-TN-D-2812
Accession Number
65N23714
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
UNSTEADY FLOW
DIGITAL COMPUTER
LIQUID FLOW
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