ACTIVE CONTROL OF FLOW SEPARATION OVER SUPERCRITICAL AIRFOIL USING SYNTHETIC JET /
Сохранить в:
| Главный автор: | |
|---|---|
| Соавтор: | |
| Другие авторы: | , |
| Формат: | |
| Язык: | английский |
| Опубликовано: |
Dhaka :
ME DEPT. MIST,
c2024.
|
| Предметы: | |
| Метки: |
Нет меток, Требуется 1-ая метка записи!
|
Схожие документы: ACTIVE CONTROL OF FLOW SEPARATION OVER SUPERCRITICAL AIRFOIL USING SYNTHETIC JET /
- MACHINE LEARNING APPROACH TO SHOCK DETECTION IN COMPRESSIBLE FLOW OVER A WEDGE /
- STUDY OF IMPACT OF JET ON DIFFERENT VANES FOR MEASURING FLOW RATE AND IMPACT FORCE /
- SYNERGISTIC FLOW CONTROL: INGRATION OF DYNAMIC VORTEX GENERATORS AND VARYING DIMPLE GEOMETRIES FOR ENHANCED AERODYNAMIC CHARACTERISTICS FOR NACA 2412 AIRFOIL /
- NUMERICAL INVESTIGATION OF LIFT AUGMENTATION WITH CO-FLOW JET AIRFOIL /
- Active Control of Noise and Vibration : Volume I /
- Active Control of Noise and Vibration : Volume II /