Interaction of a shock wave with the sonic line

DOI

https://doi.org/10.1007/978-94-010-0017-8_3
Final published version

A. G. Kuz'min

The paper addresses patterns of interaction of shock waves with the sonic line. The incident shocks are formed by either a small curvature of an airfoil arc, or a small step in its contour, or a short bump superposed on the airfoil. We analyse the structure of inviscid steady flow and discuss its instability at certain boundary conditions.

Original language	English
Title of host publication	IUTAM Symposium Transsonicum IV
Editors	H. SOBIECZKY
Pages	13-18
Number of pages	6
DOIs	https://doi.org/10.1007/978-94-010-0017-8_3
State	Published - 1 Dec 2003

Publication series

Name	Fluid Mechanics and its Applications
Volume	73
ISSN (Print)	0926-5112

Scopus subject areas

Mechanics of Materials
Mechanical Engineering
Fluid Flow and Transfer Processes

ID: 38435280