Infinite-thin shock layer solutions for stationary compressible conical flows and numerical results via Fourier spectral method
DOI10.1137/23M1566820MaRDI QIDQ6641693
Xueying Su, Hairong Yuan, Aifang Qu
Publication date: 21 November 2024
Published in: SIAM Journal on Applied Mathematics (Search for Journal in Brave)
supersonic flowChaplygin gasFourier spectral methodconical flowsingular ODERadon measure solutioninfinite-thin shock layer
Hyperbolic conservation laws (35L65) Numerical solution of boundary value problems involving ordinary differential equations (65L10) Hypersonic flows (76K05) Euler equations (35Q31) PDEs on manifolds (35R01) PDEs with measure (35R06)
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