DEVELOPMENT OF A CFD MODEL FOR SIMULATING THE AERODYNAMIC PERFORMANCE OF A BLENDED WING BODY AIRCRAFT (WITH AND WITHOUT VORTEX GENERATOR) /
محفوظ في:
| المؤلف الرئيسي: | |
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| مؤلف مشترك: | |
| مؤلفون آخرون: | , |
| التنسيق: | كتاب |
| اللغة: | الإنجليزية |
| منشور في: |
Dhaka :
AE DEPT. MIST,
c2024.
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| الموضوعات: | |
| الوسوم: |
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
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مواد مشابهة: DEVELOPMENT OF A CFD MODEL FOR SIMULATING THE AERODYNAMIC PERFORMANCE OF A BLENDED WING BODY AIRCRAFT (WITH AND WITHOUT VORTEX GENERATOR) /
- ANALYSIS OF AERODYNAMIC PERFORMANCE OF BLENDED WING BODY WITH VORTEX GENERATORS AND WINGLETS /
- EXPERIMENTAL STUDY ON THE EFFECT OF DIFFERENT WINGLET CONFIGURATIONS ON THE LIFT AND DRAG CHARACTERISTICS OF A BLENDED WING BODY AIRCRAFT
- EXPERIMENTAL STUDY ON THE EFFECT OF DIFFERENT WINGLET CONFIGURATIONS ON THE LIFT AND DRAG CHARACTERISTICS OF A BLENDED WING BODY AIRCRAFT /
- COMPARATIVE STUDY OF SHELL & TUBE HEAT EXCHANGER PERFORMANCE WITH & WITHOUT DELTA WINGLET VORTEX GENERATORS /
- CFD SIMULATION OF FLOW AROUND 3D SUBMARINE SHAPED BODY
- PASSIVE CONTROL OF WING ROCK IN A DELTA WING AIRCRAFT /