1994
DOI: 10.1063/1.868307
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Fanno processes in dense gases

Abstract: The global behavior of Fanno processes is examined for dense gases. It is shown that three sonic points corresponding to two local maxima and one local minimum in the entropy can occur if the fluid is of the Bethe-Zel'dovich-Thompson type. Both analytical and numerical examples of the nonclassical behavior are provided.

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Cited by 11 publications
(2 citation statements)
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References 19 publications
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“…Afterwards, Kluwick (1993) discussed the viscous and real gas interaction for a transonic nozzle, after using the small-perturbation technique and explored the non-classical fluid effects on the throat geometry and the shock-wave formation. Cramer & Fry (1993) used a similar approach for the evaluation of non-classical expansion in inviscid nozzles, and in a different work Cramer, Monaco & Fabeny (1994) evaluated the Fanno flows of non-ideal dense gases. In this same trend Schnerr & Leidner (1994) presented a rigorous evaluation of internal flows with multiple sonic points, which occurred in non-classical flows.…”
Section: Introductionmentioning
confidence: 99%
“…Afterwards, Kluwick (1993) discussed the viscous and real gas interaction for a transonic nozzle, after using the small-perturbation technique and explored the non-classical fluid effects on the throat geometry and the shock-wave formation. Cramer & Fry (1993) used a similar approach for the evaluation of non-classical expansion in inviscid nozzles, and in a different work Cramer, Monaco & Fabeny (1994) evaluated the Fanno flows of non-ideal dense gases. In this same trend Schnerr & Leidner (1994) presented a rigorous evaluation of internal flows with multiple sonic points, which occurred in non-classical flows.…”
Section: Introductionmentioning
confidence: 99%
“…Similar split-shock configurations have also been predicted in nozzle flows 5,6 and Fanno flows. 7 Shock splitting has also been described in the context of the existence and disintegration of compression shocks by Cramer 12 and Menikoff and Plohr. 16 In order to provide an example of the representation of shocked Rayleigh flows in the p-V plane we have sketched the Q vs V curve and the Rayleigh line and shock adiabats corresponding to the split-shock flow 02-5-b-10-11-a in Figs.…”
Section: -11mentioning
confidence: 99%