1967
DOI: 10.1007/bf00634559
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Berechnung der Str�mung in Lavald�sen mit beliebig verteilter W�rmezufuhr

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Cited by 11 publications
(3 citation statements)
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“…Without entering into the difficult analysis of the supercritical flow solution, we attempt to set up a criterion that can predict whether or not for given initial reservoir conditions, nozzle geometry and Q~,,(x) the flow is supercritical. We restrict our discussion to supersonic heat addition (Xb > O) because subsonic heat addition (Xb < 0) requires the influence of the exit boundary conditions as well [for numerical solution of the differential theory with heat addition in the subsonic region see Jungclaus and van Raay (1967)]. It follows at once from Proposition 2.2.2 that the flow is subcritical if…”
Section: Cpo To Cpo Tomentioning
confidence: 99%
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“…Without entering into the difficult analysis of the supercritical flow solution, we attempt to set up a criterion that can predict whether or not for given initial reservoir conditions, nozzle geometry and Q~,,(x) the flow is supercritical. We restrict our discussion to supersonic heat addition (Xb > O) because subsonic heat addition (Xb < 0) requires the influence of the exit boundary conditions as well [for numerical solution of the differential theory with heat addition in the subsonic region see Jungclaus and van Raay (1967)]. It follows at once from Proposition 2.2.2 that the flow is subcritical if…”
Section: Cpo To Cpo Tomentioning
confidence: 99%
“…(45)- (48) requires consideration of the nonequilibrium rate equation if g'r 0 and can only be achieved by numerical analysis. The numerical solutions of the system corresponding to heat addition from internal sources and from nonequilibrium condensation of wet steam are already available in the literature from the work of Jungclaus and van Raay (1967) and Barschdorff (1971). A better understanding of the nature of solution can be achieved qualitatively by applying the singularity theory of differential equations [e.g.…”
Section: Differential Theory Of Nozzle Flows With Heat Addition From mentioning
confidence: 99%
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