2003
DOI: 10.1007/s00220-003-0909-2
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Asymptotic Stability of the Stationary Solution to the Compressible Navier–Stokes Equations in the Half Space

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Cited by 129 publications
(134 citation statements)
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“…We shall investigate the asymptotic stability of the rarefaction wave, the boundary layer solution and their combination. Unlike the outflow problem, the velocity u − on the boundary for the inflow problem is positive which is not good for the analysis, we have to estimate more boundary terms than those of [16].…”
Section: Case 3 (Positive Velocity On the Boundary)mentioning
confidence: 99%
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“…We shall investigate the asymptotic stability of the rarefaction wave, the boundary layer solution and their combination. Unlike the outflow problem, the velocity u − on the boundary for the inflow problem is positive which is not good for the analysis, we have to estimate more boundary terms than those of [16].…”
Section: Case 3 (Positive Velocity On the Boundary)mentioning
confidence: 99%
“…Comparing with isentropic gas, the boundary conditions for the full compressible Navier-Stokes system become more complicated and analytically it is more difficult to control the terms coming from the boundary. More recently, Kawashima and Zhu [16] investigated the existence of the boundary layer solution and its asymptotic stability for the outflow problem of (1.1) in which the sign of the velocity u − on the boundary is negative, which plays a key role in the a priori estimate. In this paper we focus our attention on the impermeable wall problem and inflow problem.…”
Section: Case 3 (Positive Velocity On the Boundary)mentioning
confidence: 99%
“…Only the results rigorously proved concerning above asymptotic behaviors are given by Kawashima & Nishibata [1]. They proved that if w+ G Qj U p er i W-G BL(w+), and \w+ -w-\ is suitably small, then the boundary layer solution W BL (x',W-,w+) is asymptotically stable.…”
Section: Suppose U-> 0 and W+ G Bl(w-) I) If W-gmentioning
confidence: 99%
“…which is simply equivalent to u+ < U-in our cases, we can define the shock curves S\(w-) and S2(w-) for any fixed left state W-G fi by =1 , that is, RR(w-) with the boundary Ri(w-) and /^(w-), RS(w-) with the boundary Ri(w-) and 52(^_), SR{w-) with the boundary Si(w-) and R2(w-) 1 and SS(w-) with the boundary Si^-) and 82 (11) …”
Section: U4 -V-mentioning
confidence: 99%
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