COMPUTATIONAL ANALYSIS OF THE EFFECT OF DIFFERENT SHAPED DIMPLES WITH VARYING LOCATION ON THE AERODYNAMICS EFFICIENCY OF NACA 0012 AIRFOIL /
Kaydedildi:
| Yazar: | |
|---|---|
| Müşterek Yazar: | |
| Diğer Yazarlar: | , |
| Materyal Türü: | Kitap |
| Dil: | İngilizce |
| Baskı/Yayın Bilgisi: |
Dhaka :
AE DEPT. MIST,
c2020.
|
| Konular: | |
| Etiketler: |
Etiket eklenmemiş, İlk siz ekleyin!
|
Benzer Materyaller: 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