A NUMERICAL ANALYSIS ON THE AERODYNAMIC CHARACTERISTICS OF NACA 0015 AND NACA 2412 AEROFOILS WITH CURVED TRAILING-EDEG PLANFORM /
保存先:
| 第一著者: | |
|---|---|
| 団体著者: | |
| その他の著者: | , , |
| フォーマット: | 図書 |
| 言語: | 英語 |
| 出版事項: |
Dhaka :
AE DEPT. MIST,
c2022.
|
| 主題: | |
| タグ: |
タグなし, このレコードへの初めてのタグを付けませんか!
|
類似資料: A NUMERICAL ANALYSIS ON THE AERODYNAMIC CHARACTERISTICS OF NACA 0015 AND NACA 2412 AEROFOILS WITH CURVED TRAILING-EDEG PLANFORM /
- CHARACTERISTIC ANALYSIS OF NACA 0018 AND NACA 2412 AIRFOIL WITH LEADING EDGE AND TRAILING EDGE ROTATING CYLINDER /
- A COMPARATIVE STUDY OF AERODYNAMIC CHARACTERISTICS OF NACA 0015 AND NACA 4415 AIRFOILS AT VARIOUS REYNOLDS NUMBER /
- COMPARATIVE STUDY OF BLOWING AND SUCTION SLOT GEOMETRY OPTIMIZATION ON NACA 0015 AND NACA 2412 AIRFOIL /
- STUDY AND COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS AND IMPROVED PERFORMANCE OF NACA 0015 AIRFOIL WITH BLEED /
- EXPERIMENTAL STUDY OF FLOW VELOCITY AND DIRECTION AROUND NACA 0012 & NACA 0015 AIRFOIL /
- STUDY OF THE FLOW FIELD ON THE UPPER SURFACE OF NACA 0015 & NACA 2418 AT DIFFERENT AANGLE OF ATTACK /