AERODYNAMIC PERFORMANCE ANALYSIS AND PROPULSION SYSTEM DESIGN OF AN UNMANNED AERIAL VEHICLE USING NACA 4415 PROFILE / LT Tarik, LT Nabila, Nayeema parvin .
محفوظ في:
| المؤلف الرئيسي: | |
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| مؤلف مشترك: | |
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| التنسيق: | كتاب |
| اللغة: | الإنجليزية |
| منشور في: |
Dhaka :
ME DEPT MIST ,
c 2014 .
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| الموضوعات: | |
| الوسوم: |
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مواد مشابهة: AERODYNAMIC PERFORMANCE ANALYSIS AND PROPULSION SYSTEM DESIGN OF AN UNMANNED AERIAL VEHICLE USING NACA 4415 PROFILE /
- ''DESIGN DEVELOPMENT AND PERFORMANCE ANALYSIS OF THE PROPULSION SYSTEM OF A SHORT RANGE UNMANNED AERIAL VEHICLE''
- "DESIGN FABRICATION,DEVELOPMENT AND PERFORMANCE ANALYSIS OF THE PROPULSION SYSTEM OF A SMALL SURVEILLANCE UNMANNED AERIAL VEHICLE" /
- A COMPARATIVE STUDY OF AERODYNAMIC CHARACTERISTICS OF NACA 0015 AND NACA 4415 AIRFOILS AT VARIOUS REYNOLDS NUMBER /
- DESIGN OF A FIXED WING JET PROPULSION POWERED UNMANNED AERIAL VEHICLE (UAV) TARGET DRONE /
- DESIGN AND FABRICATION OF AN UNMANNED AERIAL VEHICLE EATABLE OF DELIVERING MISSION PAYLOAD /
- "DESIGN,FABRICATION AND DEVELOPMENT OF AN UNMANNED AERIAL VEHICLE CAPABLE OF DELIVERING MISSION PAYLOAD"