PASSIVE CONTROL OF WING ROCK IN A DELTA WING AIRCRAFT /
محفوظ في:
| المؤلف الرئيسي: | |
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| مؤلف مشترك: | |
| التنسيق: | كتاب |
| اللغة: | الإنجليزية |
| منشور في: |
Dhaka :
AE DEPT. MIST,
c2025.
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| الموضوعات: | |
| الوسوم: |
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
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مواد مشابهة: PASSIVE CONTROL OF WING ROCK IN A DELTA WING AIRCRAFT /
- STUDENT ANALYSIS OF AIRCRAFT WINGS WITH VARIOUS CONDITIONS /
- PERFORMANCE OPTIMIZATION OF A VARIABLE GEOMETRICAL WING:ANALYSIS AND DESIGN OF MORPHING WING FOR UNMANNED AERIAL VEHICLE /
- ANALYZING AERO-STRUCTURAL BEHAVIOUR OF CONVENTIONAL AIRCRAFT WINGS THROUGH COMPUTATIONAL APPROACH AND EXPERIMENTAL VALIDATION /
- 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 A CFD MODEL FOR SIMULATING THE AERODYNAMIC PERFORMANCE OF A BLENDED WING BODY AIRCRAFT (WITH AND WITHOUT VORTEX GENERATOR) /