2014
DOI: 10.1007/s00205-014-0738-9
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Interaction of Rarefaction Waves and Vacuum in a Convex Duct

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Cited by 17 publications
(10 citation statements)
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“…Remark 5. For the case that Riemann invariants are both constants on Γ in which is a straight segment vertical to the velocity of the incoming flow, the problem has been solved by Chen and Qu in [5]. Here we extend their work to a more general case.…”
Section: Remarkmentioning
confidence: 89%
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“…Remark 5. For the case that Riemann invariants are both constants on Γ in which is a straight segment vertical to the velocity of the incoming flow, the problem has been solved by Chen and Qu in [5]. Here we extend their work to a more general case.…”
Section: Remarkmentioning
confidence: 89%
“…On the other hand, if the rotation is involved, in the general case, due to the possible compression of gases, the smooth solutions will blow up and the shock is formed (see [6], [20], [21] and [23]). Meanwhile, if the gases are suitably expanded or expanded into the vacuum, the global solutions can exist(see [4], [5], [10], [11], [22], [24] and [27]- [29]).…”
Section: Remark 3 For the M-d Compressiblementioning
confidence: 99%
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“…(1.9) see Figure 2. Global smooth isentropic irrotational supersonic flows in the semi-infinite divergent duct were constructed in [2,14,15]. In [15], the authors also constructed a global smooth transonic solution in a De Laval nozzle.…”
Section: Introductionmentioning
confidence: 99%
“…In order to prove that the global solution can be constructed after solving a finite number of Gourst problems and slip boundary problems, the method of hodograph transformation in [2] does not work here, since we do not have Riemann invariants for the 2D steady full Euler system. In this paper, we use characteristic angles α and β.…”
Section: Introductionmentioning
confidence: 99%