STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY LAYER CONTROL ( MSBC) ON SINGLE & DOUBLE CYLINDER CONFIGURATION NACA 23018 AIRFOIL /
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| Format: | Knjiga |
| Jezik: | engleski |
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AE DEPT MIST ,
C 2018.
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Slični predmeti: 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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- STUDY AND COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS BETWEEN DIFFERENT CONFIGURATIONS OF THREE DIMENSIONAL MODELS OF NACA 4412 AIRFOIL /