Inviscid compressible flow with shock in two-dimensional slender nozzles

DOI10.1017/S0022112085002373zbMath0576.76059MaRDI QIDQ3696739

No author found.

Publication date: 1985

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

zbMATH Keywords

subsonic flowasymptotic-expansion methodinviscid compressible flows with shockinviscid shock-induced separationtwo-dimensional slender nozzles

Mathematics Subject Classification ID

Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10) Supersonic flows (76J20)

Cites Work

• On the flow near a weak shock wave downstream of a nozzle throat

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