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Shock/shock and shock/boundary layer interactions in an axisymmetric steady laminar flow

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Publication:706389
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DOI10.1007/s00193-003-0187-0zbMath1063.76584OpenAlexW2031449927MaRDI QIDQ706389

Yves Burtschell, David E. Zeitoun

Publication date: 8 February 2005

Published in: Shock Waves (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00193-003-0187-0


zbMATH Keywords

Riemann solverAUSM+ solver


Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Shock waves and blast waves in fluid mechanics (76L05) Finite volume methods applied to problems in fluid mechanics (76M12)


Related Items (3)

Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows ⋮ \(H_{2}\) injection and combustion in a Mach 5 air inlet through a viscous Mach interaction ⋮ Axisymmetric shock wave interaction with a cone: a benchmark test




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