COMPUTATIONAL ANALYSIS OF THE EFFECT OF DIFFERENT SHAPED DIMPLES WITH VARYING LOCATION ON THE AERODYNAMICS EFFICIENCY OF NACA 0012 AIRFOIL /
সংরক্ষণ করুন:
| প্রধান লেখক: | |
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| সংস্থা লেখক: | |
| অন্যান্য লেখক: | , |
| বিন্যাস: | গ্রন্থ |
| ভাষা: | ইংরেজি |
| প্রকাশিত: |
Dhaka :
AE DEPT. MIST,
c2020.
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| বিষয়গুলি: | |
| ট্যাগগুলো: |
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অনুরূপ উপাদানগুলি: 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