Hysteresis Phenomena in Reflection of Shock Waves

G. Ben-Dor

doi:10.1007/978-3-319-16835-7_1

Hysteresis Phenomena in Reflection of Shock Waves

G. Ben-Dor

Department of Mechanical Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

When a supersonic flow,M0 >1, encounters a straight compressive wedge a straight and attached to the leading edge of the reflecting wedge shock wave is formed provided the reflecting wedge angle is smaller than the maximum flow deflection angle appropriate to flow-Mach number, M0.

Original language	English
Title of host publication	29th International Symposium on Shock Waves 1, ISBN 978-3-319-16834-0. Springer International Publishing Switzerland, 2015
Pages	3-10
DOIs	https://doi.org/10.1007/978-3-319-16835-7_1
State	Published - 2015

Keywords

Physics

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10.1007/978-3-319-16835-7_1

http://adsabs.harvard.edu/abs/2015shw1.conf....3B

Cite this

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title = "Hysteresis Phenomena in Reflection of Shock Waves",

abstract = "When a supersonic flow,M0 >1, encounters a straight compressive wedge a straight and attached to the leading edge of the reflecting wedge shock wave is formed provided the reflecting wedge angle is smaller than the maximum flow deflection angle appropriate to flow-Mach number, M0.",

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author = "G. Ben-Dor",

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AB - When a supersonic flow,M0 >1, encounters a straight compressive wedge a straight and attached to the leading edge of the reflecting wedge shock wave is formed provided the reflecting wedge angle is smaller than the maximum flow deflection angle appropriate to flow-Mach number, M0.

KW - Physics

U2 - 10.1007/978-3-319-16835-7_1

DO - 10.1007/978-3-319-16835-7_1

M3 - Conference contribution

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EP - 10

BT - 29th International Symposium on Shock Waves 1, ISBN 978-3-319-16834-0. Springer International Publishing Switzerland, 2015

ER -

Hysteresis Phenomena in Reflection of Shock Waves

Abstract

Keywords

Access to Document

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Cite this