EFFECT OF MOMENTUM INJECTION ON THE PERFORMANCE OF AIRFOIL (MOVING SURFACE BOUNDARY LAYER CONTROL /
में बचाया:
| मुख्य लेखक: | |
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| निगमित लेखक: | |
| अन्य लेखक: | , , , |
| स्वरूप: | पुस्तक |
| भाषा: | अंग्रेज़ी |
| प्रकाशित: |
Dhaka :
AE DEPT MIST ,
C 2017 .
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| विषय: | |
| टैग: |
कोई टैग नहीं, इस रिकॉर्ड को टैग करने वाले पहले व्यक्ति बनें!
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समान संसाधन: EFFECT OF MOMENTUM INJECTION ON THE PERFORMANCE OF AIRFOIL (MOVING SURFACE BOUNDARY LAYER CONTROL /
- 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 /
- Boundary layer theory
- DESIGN AND OPTIMIZATION OF LOW SPEED WIND TURBINE WITH MOMENTUM INJECTION /
- An experimental and numerical investigation on boundary layer control with blown flaps incorporating Coanda effect
- STUDY OF MOMENTUM INJENCTION: EFFECT OF CLEARENCE BETWEEN ROTATING CYLINDER AND GROOVED AIRFOIL /