STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY LAYER CONTROL ( MSBC) ON SINGLE & DOUBLE CYLINDER CONFIGURATION NACA 23018 AIRFOIL /
שמור ב:
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| מחבר תאגידי: | |
| מחברים אחרים: | , , |
| פורמט: | ספר |
| שפה: | אנגלית |
| יצא לאור: |
Dhaka :
AE DEPT MIST ,
C 2018.
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| תגים: |
אין תגיות, היה/י הראשונ/ה לתייג את הרשומה!
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פריטים דומים: STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY LAYER CONTROL ( MSBC) ON SINGLE & DOUBLE CYLINDER CONFIGURATION NACA 23018 AIRFOIL /
- STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY-LAYER CONTROL (MSBC) ON A DOUBLE CYLINDER CONFIGURATION : NACA 0018 AIRFOIL /
- EFFECT OF MOMENTUM INJECTION ON THE PERFORMANCE OF AIRFOIL (MOVING SURFACE BOUNDARY LAYER CONTROL /
- Boundary layer theory
- CHARACTERISTIC ANALYSIS OF NACA 0018 AND NACA 2412 AIRFOIL WITH LEADING EDGE AND TRAILING EDGE ROTATING CYLINDER /
- AERODYNAMICS PERFORMANCE ANALYSIS OF 2D AIRFOIL/ NACA 4418 INCORPORATING WITH ROTATING CYLINDER /
- STUDY AND COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS BETWEEN DIFFERENT CONFIGURATIONS OF THREE DIMENSIONAL MODELS OF NACA 4412 AIRFOIL /