As a result of a large number of numerical and experimental investigations performed
during last 5 years in the Institute of Theoretical and Applied Mechanics (Novosibirsk), it
has been established that the transition can be accompanied by a hysteresis, i.e. the angles
of the direct and reverse transition can be different. The influence of free-stream disturbances
and the 3D effects, which are unavoidable in experiments, have been studied. It has been shown
numerically that so-called peripheral Mach reflection always takes place, even if the reflection
in the center is regular. When the reflection is Mach one throughout the whole span, the Mach
stem height can vary non-monotonously along the spanwise direction. The existence of an intermittent
reflection is also possible. In this case, the reflection in the center is Mach one,
closer to the periphery it is regular, and at the far periphery it is Mach one again.
All these results have been confirmed experimentally when the 3D structure of shock waves
has been visualized with the laser sheet method.
Note. Abstracts are published in author's edition
© 1996-2001, Institute of computational Techologies SB RAS, Novosibirsk
© 1996-2001, Siberian Branch of Russian Academy of Science, Novosibirsk