About permissible limits at assignment of boundary effect following the shock wave
Автор: Adrianov A.L.
Журнал: Сибирский аэрокосмический журнал @vestnik-sibsau
Рубрика: Математика, механика, информатика
Статья в выпуске: 5 (45), 2012 года.
Бесплатный доступ
The author considers influence of boundary effect following the shock wave on evolution of the shock wave itself, when it penetrates the shift layer. Permissible limits at assignment of boundary effect are revealed. Concepts of Uskov’s invariant and angle are introduced.
Strong and weak gas-dynamic blowout, boundary effect, shock wave, extended differential conditions on a shock wave, mach's and uskov's angles
Короткий адрес: https://sciup.org/148176971
IDR: 148176971
Статья научная
