2012
DOI: 10.1016/s0252-9602(12)60064-2
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The riemann problem with delta initial data for the one-dimensional chaplygin gas equations

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Cited by 27 publications
(2 citation statements)
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“…As for delta shock waves, we refer readers to [19,20,21,30,32], and the references cited therein for more details. We can also see such as [6,17,33] for the related results about the system (1)-(2) with β = 0. In this paper, we are concerned with Chaplygin gas equations with a source term (β = 0) such as damping, friction and relaxation effect.…”
Section: Lihui Guo Tong LI and Gan Yinmentioning
confidence: 78%
“…As for delta shock waves, we refer readers to [19,20,21,30,32], and the references cited therein for more details. We can also see such as [6,17,33] for the related results about the system (1)-(2) with β = 0. In this paper, we are concerned with Chaplygin gas equations with a source term (β = 0) such as damping, friction and relaxation effect.…”
Section: Lihui Guo Tong LI and Gan Yinmentioning
confidence: 78%
“…The main difficulty of studying limiting hypersonic flows is a proper definition of Radon measure solutions of initial-boundary value problems of compressible Euler equations. We note that there are many works on the Cauchy problems of unsteady Euler equations of pressureless flow or Chaplygin gas, and other singular hyperbolic conservation laws for initial value problems, mainly motivated by mathematical curiosity (see, for example, [11,12,23,22,28] and references therein). These works present different definitions of measure solutions of hyperbolic conservation laws.…”
Section: Hypersonic-limit Euler Flows Passing Cones 2667mentioning
confidence: 99%