DESIGN AND COMPUTATIONAL ANALYSIS OF SUBSONIC LOITER MUNITION'S WING USING DIFFERENT AIRFOIL SECTION /
Saved in:
| 主要作者: | |
|---|---|
| 企业作者: | |
| 其他作者: | , |
| 格式: | 图书 |
| 语言: | 英语 |
| 出版: |
Dhaka :
AE DEPT. MIST,
c2026.
|
| 主题: | |
| 标签: |
没有标签, 成为第一个标记此记录!
|
相似书籍: DESIGN AND COMPUTATIONAL ANALYSIS OF SUBSONIC LOITER MUNITION'S WING USING DIFFERENT AIRFOIL SECTION /
- PERFORMANCE ANALYSIS OF FIXED AND MORPHING WINGS USING NACA 4412 ASYMMETRIC AIRFOILS UNDER VARYING ANGLES OF ATTACK AND FLOW REGIMES /
- EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF DIFFERENT CHEVRON NOZZLES /
- LARGE DEFECTION ANALYSIS OF AN AIRCRAFT WING WITH ELLIPTICAL LIFT DISTRIBUTION AT DIFFERENT FLIGHT CONDITION /
- DESIGN OF A CLOSED LOOP SUBSONIC WIND TUNNEL /
- PASSIVE CONTROL OF WING ROCK IN A DELTA WING AIRCRAFT /
- SURFACE MODIFICATION OF NACA 4418 AIRFOIL WITH DIFFERENT SHAPED DIMPLES AND AERODYNAMIC PERFORMANCE ANALYSIS /