STRUCTURAL DESIGN ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE /
محفوظ في:
| مؤلف مشترك: | |
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| مؤلفون آخرون: | , |
| التنسيق: | كتاب |
| اللغة: | الإنجليزية |
| منشور في: |
Dhaka :
ME DEPT. MIST,
c2014.
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| الموضوعات: | |
| الوسوم: |
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مواد مشابهة: STRUCTURAL DESIGN ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE /
- STRUCTURAL DESIGN, ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE
- INVESTIGATION OF THE EFFECT OF DIFFERENT AIRFOIL SHAPED FUSELAGE ON THE PERFORMANCE OF AN UNMANNED AIR VEHICLE /
- EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF THE CHARACTERISTICS OF NACA 4412 AEROFOIL USING DIFFERENT SHAPES /
- Development Of Design Of Aerofoil Shaped Fuselage And CFD Investigation Of Its Aerodynamic Characteristics
- DESIGN AND CONSTRUCTION OF FLAPPING WING AERIAL VEHICLE (FWAV) /
- DESIGN AND FABRICATION OF THE FUSELAGE OF A RADIO CONTROLLED AERIAL VEHICLE /