1972
DOI: 10.1115/1.3425462
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Unsteady Flow at the Junction of a Branched Duct

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Cited by 2 publications
(4 citation statements)
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“…The coefficients are taken to be constant for each value of a (see figure). Figure 6 shows the transmitted pressure ratio as a function of the incident pressure ratio in a T-junction with a section ratio equal to f. In these tests, a comparison of the calculations with experimental results (8,9) shows very good agreement. Meanwhile, the calculations are stopped for pi/po equal to 1.9 because, above this threshold, the flow becomes sonic.…”
Section: Numerical Testsmentioning
confidence: 78%
See 1 more Smart Citation
“…The coefficients are taken to be constant for each value of a (see figure). Figure 6 shows the transmitted pressure ratio as a function of the incident pressure ratio in a T-junction with a section ratio equal to f. In these tests, a comparison of the calculations with experimental results (8,9) shows very good agreement. Meanwhile, the calculations are stopped for pi/po equal to 1.9 because, above this threshold, the flow becomes sonic.…”
Section: Numerical Testsmentioning
confidence: 78%
“…The mathematical nature of the previous systems does not change when the variable pressure loss coefficients are taken to be constant. In the following sections, the coefficients are 51, 9 …”
Section: A Pressure Loss Coefficientsmentioning
confidence: 99%
“…A series of experiments conducted by Deckker with others (13,14,15) on three-pipe junctions with three different configurations has provided a useful insight into pressure wave behaviour within the junction itself but a completely theoretical analysis of the events occurring was found to be impossible. A set of diagrams was therefore produced, based on the experimental results obtained and arranged to be suitable for use in calculations employing the method of characteristics.…”
Section: The M S Was Received On 28 December 1983 and Was Acceptedformentioning
confidence: 99%
“…The velocity directions must be checked in each pipe to establish the flow type and the appropriate pair of equations is then selected from equations (1-12) above. These two equations together with the continuity equation: P l F l U l + P 2 F 2 U 2 + P 3 F 3 U 3 = 0 (13) are expressed in terms of non-dimensional parameters and solved iteratively for the three reflected Riemann variables.…”
Section: Momentum Modelmentioning
confidence: 99%