MATEC Web of Conferences
The technique and results of the experimental-theoretical study of gas dynamics, heat transfer and the structure of gas flow in the flowing channel of a model hypersonic air-ramjet engine are presented for Mach numbers M (5; 6).
| Другие авторы: | , , , , |
|---|---|
| Формат: | Статья в сборнике |
| Язык: | English |
| Публикация: |
Les Ulis
EDP Sciences
2018
|
| Предметы: | |
| Online-ссылка: | https://doi.org/10.1051/matecconf/201819401037 http://earchive.tpu.ru/handle/11683/51462 |