ANALYZING AERO-STRUCTURAL BEHAVIOUR OF CONVENTIONAL AIRCRAFT WINGS THROUGH COMPUTATIONAL APPROACH AND EXPERIMENTAL VALIDATION /
Salvato in:
| Autore principale: | |
|---|---|
| Ente Autore: | |
| Natura: | Libro |
| Lingua: | inglese |
| Pubblicazione: |
Dhaka :
AE DEPT. MIST,
c2025.
|
| Soggetti: | |
| Tags: |
Nessun Tag, puoi essere il primo ad aggiungerne!!
|
Documenti analoghi: ANALYZING AERO-STRUCTURAL BEHAVIOUR OF CONVENTIONAL AIRCRAFT WINGS THROUGH COMPUTATIONAL APPROACH AND EXPERIMENTAL VALIDATION /
- PASSIVE CONTROL OF WING ROCK IN A DELTA WING AIRCRAFT /
- STUDENT ANALYSIS OF AIRCRAFT WINGS WITH VARIOUS CONDITIONS /
- DESIGN & FABRICATION OF WING CONTROLS,UNDERCARRIAGE AND SKIN OF HOME BUILT EXPERIMENTAL AIRCRAFT’’ MIST X-01’’ /
- EXPERIMENTAL STUDY ON THE EFFECT OF DIFFERENT WINGLET CONFIGURATIONS ON THE LIFT AND DRAG CHARACTERISTICS OF A BLENDED WING BODY AIRCRAFT /
- DEVELOPMENT OF AN EXPERIMENTAL SETUP FOR ANALYZING THE INFLUENCE OF MAGNUS EFFECT ON THE PERFORMANCE OF AIRFOIL /
- DESIGN & DEVELOPMENT OF STRUCTURE OF A PROTOTYPE AIRCRAFT MIST EXPERIMENTAL-1 / Refaty Munni, Najifa Tasnim & Asif Bin Hossain.