STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY-LAYER CONTROL (MSBC) ON A DOUBLE CYLINDER CONFIGURATION : NACA 0018 AIRFOIL /
Wedi'i Gadw mewn:
| Prif Awdur: | |
|---|---|
| Awdur Corfforaethol: | |
| Awduron Eraill: | , |
| Fformat: | Llyfr |
| Iaith: | Saesneg |
| Cyhoeddwyd: |
Dhaka :
AE DEPT MIST
c2017
|
| Pynciau: | |
| Tagiau: |
Dim Tagiau, Byddwch y cyntaf i dagio'r cofnod hwn!
|
Eitemau Tebyg: 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 /