STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY-LAYER CONTROL (MSBC) ON A DOUBLE CYLINDER CONFIGURATION : NACA 0018 AIRFOIL /
保存先:
| 第一著者: | |
|---|---|
| 団体著者: | |
| その他の著者: | , |
| フォーマット: | 図書 |
| 言語: | 英語 |
| 出版事項: |
Dhaka :
AE DEPT MIST
c2017
|
| 主題: | |
| タグ: |
タグなし, このレコードへの初めてのタグを付けませんか!
|
類似資料: 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 /