An experimental and numerical investigation on boundary layer control with blown flaps incorporating Coanda effect
Сохранить в:
| Главные авторы: | , |
|---|---|
| Формат: | |
| Язык: | английский |
| Опубликовано: |
Dhaka, Bangladesh :
Department of Mechanical Engineering, Military Institute of Science and Technology,
@ February 2023.
|
| Редактирование: | Bachelor's thesis |
| Метки: |
Нет меток, Требуется 1-ая метка записи!
|
Схожие документы: An experimental and numerical investigation on boundary layer control with blown flaps incorporating Coanda effect
- Boundary layer theory
- EFFECT OF MOMENTUM INJECTION ON THE PERFORMANCE OF AIRFOIL (MOVING SURFACE BOUNDARY LAYER CONTROL /
- AN EXPERIMENTAL AND NUMERICAL INVESTIGATION ON EFFECT OF SHAPES AND ARRANGEMENT OF SOLID BODIES IN WIND LOADING
- AN EXPERIMENTAL AND NUMERICAL INVESTIGATION ON EFFECT OF SHAPES AND ARRANGEMENT OF SOLID BODIES IN WIND LOADING /
- STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY-LAYER CONTROL (MSBC) ON A DOUBLE CYLINDER CONFIGURATION : NACA 0018 AIRFOIL /
- STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY LAYER CONTROL ( MSBC) ON SINGLE & DOUBLE CYLINDER CONFIGURATION NACA 23018 AIRFOIL /