Experimental-theoretical study of pressure distribution along the wall when a supersonic gas flow moves in an axisymmetric channel with sudden expansion
The paper describes a study of pressure distribution along the wall of an axisymmetric channel with a straight step. A supersonic gas flow formed inside the channel when an external flow with Mach numbers M = 5 and M = 6 moves around an axisymmetric model with internal duct is considered. A superson...
| Опубликовано в: : | Thermophysics and aeromechanics Vol. 29, № 1. P. 87-97 |
|---|---|
| Главный автор: | |
| Другие авторы: | , |
| Формат: | Статья в журнале |
| Язык: | English |
| Предметы: | |
| Online-ссылка: | http://vital.lib.tsu.ru/vital/access/manager/Repository/koha:001003397 |