STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY-LAYER CONTROL (MSBC) ON A DOUBLE CYLINDER CONFIGURATION : NACA 0018 AIRFOIL /
Gorde:
| Egile nagusia: | |
|---|---|
| Erakunde egilea: | |
| Beste egile batzuk: | , |
| Formatua: | Liburua |
| Hizkuntza: | ingelesa |
| Argitaratua: |
Dhaka :
AE DEPT MIST
c2017
|
| Gaiak: | |
| Etiketak: |
Etiketarik gabe, Izan zaitez lehena erregistro honi etiketa jartzen!
|
Antzeko izenburuak: 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 /
- EFFECT OF MOMENTUM INJECTION ON THE PERFORMANCE OF AIRFOIL (MOVING SURFACE BOUNDARY LAYER CONTROL /
- CHARACTERISTIC ANALYSIS OF NACA 0018 AND NACA 2412 AIRFOIL WITH LEADING EDGE AND TRAILING EDGE ROTATING CYLINDER /
- Boundary layer theory
- "INFLUENCE OF SURFACE MODIFICATION ON THE LIFT-DRAG CHARACTERISTICS OF NACA 0012 AIRFOIL" /
- AERODYNAMICS PERFORMANCE ANALYSIS OF 2D AIRFOIL/ NACA 4418 INCORPORATING WITH ROTATING CYLINDER /