DESIGN AND COMPUTATIONAL ANALYSIS OF SUBSONIC LOITER MUNITION'S WING USING DIFFERENT AIRFOIL SECTION /
Zapisane w:
| 1. autor: | |
|---|---|
| Korporacja: | |
| Kolejni autorzy: | , |
| Format: | Książka |
| Język: | angielski |
| Wydane: |
Dhaka :
AE DEPT. MIST,
c2026.
|
| Hasła przedmiotowe: | |
| Etykiety: |
Nie ma etykietki, Dołącz pierwszą etykiete!
|
Podobne zapisy: 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 /