TY - JOUR
T1 - Hysteresis Phenomena in Reflection of Shock Waves
AU - Ben-Dor, G.
PY - 2015
Y1 - 2015
N2 - 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.
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
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SP - 3
EP - 10
JO - 29th International Symposium on Shock Waves 1, ISBN 978-3-319-16834-0. Springer International Publishing Switzerland, 2015
JF - 29th International Symposium on Shock Waves 1, ISBN 978-3-319-16834-0. Springer International Publishing Switzerland, 2015
ER -