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ANALYSIS AND INSTALLATION OF AVIONICS SYSTEM IN A SMALL UNMANNED AIRCRAFT /
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DESIGN, ANALYSIS AND OPTIMIZATION OF A SMALL UNMANNED AIRCRAFT /
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DESIGN AND FABRICATION OF AN UNMANNED AERIAL VEHICLE EATABLE OF DELIVERING MISSION PAYLOAD /
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"DESIGN,FABRICATION AND DEVELOPMENT OF AN UNMANNED AERIAL VEHICLE CAPABLE OF DELIVERING MISSION PAYLOAD"
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PERFORMANCE OPTIMIZATION OF A VARIABLE GEOMETRICAL WING:ANALYSIS AND DESIGN OF MORPHING WING FOR UNMANNED AERIAL VEHICLE /
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STUDENT ANALYSIS OF AIRCRAFT WINGS WITH VARIOUS CONDITIONS /
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DESIGN PROTOTYPE PROPOSAL OF OPTICAL FIBER BASED AVIONICS DATA BUS FOR A SMALL AIRCRAFT / S.M. Easin Ankur, Faisal Ahmed & Akter Mahmud Nafi .
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A SYSTEMS ENGINEERING APPROACH TO THE DETAIL DESIGN OF TAIL,TRIM AND PERFORMANCE ANALYSIS OF A SMALL REMOTELY PILOTED AIRCRAFT /
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COMPARATIVE STUDY OF AIRCRAFT APPROACH AND LANDING PERFORMANCE USING ILS, MLS AND GLS /
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"DESIGN FABRICATION,DEVELOPMENT AND PERFORMANCE ANALYSIS OF THE PROPULSION SYSTEM OF A SMALL SURVEILLANCE UNMANNED AERIAL VEHICLE" /
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LARGE DEFECTION ANALYSIS OF AN AIRCRAFT WING WITH ELLIPTICAL LIFT DISTRIBUTION AT DIFFERENT FLIGHT CONDITION /
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DEVELOPMENT OF AIRCRAFT SYSTEM DEMONSTRATOR: FOUGA CM170 MAGISTER AIRCRAFT / Capt Arif Md. Amirul Abrar, Capt A Ashigur Rahman Sany, Hannanur Rashid Saddam.
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INVESTIGATION OF THE EFFECT OF DIFFERENT AIRFOIL SHAPED FUSELAGE ON THE PERFORMANCE OF AN UNMANNED AIR VEHICLE /
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MODELING AND SIMULATION OF LONGITUDINAL AUTOPILOT FOR GENERAL AVIATION AIRCRAFT /
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DEVELOPMENT OF A PHASED OUT AIRCRAFT AS EDUCATIONAL AID /
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DESIGN & MODELING OF RADAR CONTROL SYSTEM FOR DETECTING AIRCRAFT & MISSILE /
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AERODYNAMICS PERFORMANCE ANALYSIS OF 2D AIRFOIL/ NACA 4418 INCORPORATING WITH ROTATING CYLINDER /
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STABILITY AND PERFORMANCE ANALYSIS OF A FIXED WING (UNMANNED AERIAL VEHICLE) TARGET DRONE FOR TESTING AND AIR DEFENCE SYSTEM TARGET DRONE /
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DESIGN & DEVELOPMENT OF THRUST PROVIDER FOR A HOME BUILT AIRCRAFT (MIST-EXPERIMENTAL-1) /
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DESIGN & DEVELOPMENT OF STRUCTURE OF A PROTOTYPE AIRCRAFT MIST EXPERIMENTAL-1 / Refaty Munni, Najifa Tasnim & Asif Bin Hossain.
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ANALYSIS OF OPERATIONAL LIMIT OF AN AIRCRAFT: AN AEROELASTIC APPROACH /
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DESIGN OF CAMBERED AEROFOIL FOR UNMANNED AERIAL VEHICLE BASED ON SUBSONIC WIND TUNNEL TEXT / KH. Md. Faisal Md. Faisal Kabir, Nahian Al Hossain Basunia,
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DESIGN & FABRICATION OF WING CONTROLS,UNDERCARRIAGE AND SKIN OF HOME BUILT EXPERIMENTAL AIRCRAFT’’ MIST X-01’’ /
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DESIGN , CONSTRUCTION AND PERFORMANCE CHECKING OF BLADE ANTENNA /