Three dimensional steady subsonic Euler flows in bounded nozzles
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Publication:2442908
DOI10.1016/j.jde.2014.02.016zbMath1457.35030arXiv1305.2242OpenAlexW2143398018MaRDI QIDQ2442908
Publication date: 2 April 2014
Published in: Journal of Differential Equations (Search for Journal in Brave)
Full work available at URL: https://arxiv.org/abs/1305.2242
General aerodynamics and subsonic flows (76G25) Gas dynamics (general theory) (76N15) Hyperbolic conservation laws (35L65) A priori estimates in context of PDEs (35B45) Existence problems for PDEs: global existence, local existence, non-existence (35A01) Euler equations (35Q31) Uniqueness problems for PDEs: global uniqueness, local uniqueness, non-uniqueness (35A02) Transport equations (35Q49)
Related Items (15)
Two dimensional subsonic Euler flows past a wall or a symmetric body ⋮ Global smooth axisymmetric Euler flows with rotating effect in an infinitely long axisymmetric nozzle ⋮ Stability of spherically symmetric subsonic flows and transonic shocks under multidimensional perturbations ⋮ Subsonic Euler flows with large vorticity through an infinitely long axisymmetric nozzle ⋮ Transonic shock solutions to the Euler system in divergent-convergent nozzles ⋮ Stabilization effect of frictions for transonic shocks in steady compressible Euler flows passing three-dimensional ducts ⋮ Three dimensional non-isentropic subsonic Euler flows in rectangular nozzles ⋮ Existence and optimal convergence rates of multi-dimensional subsonic potential flows through an infinitely long nozzle with an obstacle inside ⋮ On an Elliptic Free Boundary Problem and Subsonic Jet Flows for a Given Surrounding Pressure ⋮ Subsonic divided gas flow in an infinitely long branching channel ⋮ Global smooth axisymmetric subsonic flows with nonzero swirl in an infinitely long axisymmetric nozzle ⋮ Compressible subsonic impinging flows ⋮ A deformation-curl-Poisson decomposition to the three dimensional steady Euler-Poisson system with applications ⋮ Subsonic non-isentropic Euler flows with large vorticity in axisymmetric nozzles ⋮ Subsonic Flows Past a Profile with a Vortex Line at the Trailing Edge
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