COMPUTATIONAL ANALYSIS OF THE EFFECT OF DIFFERENT SHAPED DIMPLES WITH VARYING LOCATION ON THE AERODYNAMICS EFFICIENCY OF NACA 0012 AIRFOIL /
में बचाया:
| मुख्य लेखक: | |
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| निगमित लेखक: | |
| अन्य लेखक: | , |
| स्वरूप: | पुस्तक |
| भाषा: | अंग्रेज़ी |
| प्रकाशित: |
Dhaka :
AE DEPT. MIST,
c2020.
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| विषय: | |
| टैग: |
कोई टैग नहीं, इस रिकॉर्ड को टैग करने वाले पहले व्यक्ति बनें!
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समान संसाधन: COMPUTATIONAL ANALYSIS OF THE EFFECT OF DIFFERENT SHAPED DIMPLES WITH VARYING LOCATION ON THE AERODYNAMICS EFFICIENCY OF NACA 0012 AIRFOIL /
- SURFACE MODIFICATION OF NACA 4418 AIRFOIL WITH DIFFERENT SHAPED DIMPLES AND AERODYNAMIC PERFORMANCE ANALYSIS /
- SYNERGISTIC FLOW CONTROL: INGRATION OF DYNAMIC VORTEX GENERATORS AND VARYING DIMPLE GEOMETRIES FOR ENHANCED AERODYNAMIC CHARACTERISTICS FOR NACA 2412 AIRFOIL /
- A COMPARISON OF EXPERIMENTAL WITH SIMULATION EFFECTIVE OF NACA 0012 AIRFOIL WITH BARE /
- EXPERIMENTAL STUDY OF AERODYNAMIC CO-EFFICIENTS, CO-EFFICIENT OF PRESSURE AND-FIELD AROUND 0012 AIRFOIL /
- EXPERIMENTAL STUDY OF FLOW CHARACTERISTICS AROUND NACA 4418 AND NACA 0012 AIRFOIL /
- EXPERIMENTAL STUDY OF FLOW VELOCITY AND DIRECTION AROUND NACA 0012 & NACA 0015 AIRFOIL