DESIGN AND COMPUTATIONAL ANALYSIS OF SUBSONIC LOITER MUNITION'S WING USING DIFFERENT AIRFOIL SECTION /
Αποθηκεύτηκε σε:
| Κύριος συγγραφέας: | |
|---|---|
| Συγγραφή απο Οργανισμό/Αρχή: | |
| Άλλοι συγγραφείς: | , |
| Μορφή: | Βιβλίο |
| Γλώσσα: | Αγγλικά |
| Έκδοση: |
Dhaka :
AE DEPT. MIST,
c2026.
|
| Θέματα: | |
| Ετικέτες: |
Δεν υπάρχουν, Καταχωρήστε ετικέτα πρώτοι!
|
Παρόμοια τεκμήρια: 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 /