STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY LAYER CONTROL ( MSBC) ON SINGLE & DOUBLE CYLINDER CONFIGURATION NACA 23018 AIRFOIL /
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| Andere auteurs: | , , |
| Formaat: | Boek |
| Taal: | Engels |
| Gepubliceerd in: |
Dhaka :
AE DEPT MIST ,
C 2018.
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Gelijkaardige items: 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
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