On the structure of subsonic flow between an asymmetric body and a detached shock wave

DOI10.1016/0021-8928(93)90149-GzbMath0797.76040OpenAlexW1998882350MaRDI QIDQ1324817

A. I. Rylov

Publication date: 19 July 1994

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-8928(93)90149-g

zbMATH Keywords

vortex flowconvex leading edgesconvexity of the subsonic sectionfamily of isoclines

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05)

Related Items (3)

Unnamed Item ⋮ The monotonicity properties of the solutions of first-order elliptic systems and their applications to the equations of fluid and gas mechanics ⋮ The monotonicity properties of some axisymmetric subsonic flows

Cites Work

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• On the possible modes of flow around tapered bodies of finite thickness at arbitrary supersonic velocities of the approach stream
• On certain properties of a subsonic flow behind a shock wave arising during supersonic flow around bodies of finite thickness

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