COMPUTATIONAL ANALYSIS OF THE EFFECT OF DIFFERENT SHAPED DIMPLES WITH VARYING LOCATION ON THE AERODYNAMICS EFFICIENCY OF NACA 0012 AIRFOIL /
Đã lưu trong:
| Tác giả chính: | |
|---|---|
| Tác giả của công ty: | |
| Tác giả khác: | , |
| Định dạng: | Sách |
| Ngôn ngữ: | Tiếng Anh |
| Được phát hành: |
Dhaka :
AE DEPT. MIST,
c2020.
|
| Những chủ đề: | |
| Các nhãn: |
Không có thẻ, Là người đầu tiên thẻ bản ghi này!
|
Những quyển sách tương tự: 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