Submerged shocks in conical gas flows in the presence of a mach shock-wave configurationстатья
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Дата последнего поиска статьи во внешних источниках: 25 декабря 2013 г.
Авторы:
Ostapenko N.A. ,
Chulkov A.A.
Журнал:
Fluid Dynamics
Том:
42
Номер:
2
Год издания:
2007
Издательство:
Maik Nauka/Interperiodica Publishing
Местоположение издательства:
Russian Federation
Первая страница:
310
Последняя страница:
320
DOI:
10.1134/S0015462807020160
Аннотация:
The results of a numerical study of a new type of singularities in the Mach shock-wave structure realized in supersonic nonsymmetric conical flows over V-wings with a bow shock attached to the leading edges are presented. Within the framework of the ideal gas model we study the changes in the shock system on transition, with increase in the sweep angle, from the region of nonsymmetric Mach interaction of the shocks attached to the leading edges of the wing to the region of special flow patterns, where on the windward cantilever surface a rarefaction flow is realized rather than a flow with an internal shock. It is shown, in particular, that in the region with special wing flow patterns a Mach system of shocks with a submerged shock proceeding from the branch point above the windward cantilever may exist. © Pleiades Publishing, Ltd. 2007.
Добавил в систему:
Остапенко Николай Андреевич