Design and Analysis of a Base Bleed Unit for the Drag Reduction of a High-Power Rocket Operating at Transonic Speeds
In the present study, a passive flow device is considered for drag reduction purposes through implementation in a transonic high-power rocket. The high-power rocket serves as a reference platform that, apart from the operating conditions, enforces several constraints in terms of available volume and...
Сохранить в:
| Главные авторы: | , , , , |
|---|---|
| Формат: | Artigo |
| Язык: | Inglês |
| Опубликовано: |
MDPI AG
2024-05-01
|
| Серии: | Aerospace |
| Предметы: | |
| Online-ссылка: | https://www.mdpi.com/2226-4310/11/5/385 |
| Метки: |
Нет меток, Требуется 1-ая метка записи!
|