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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 /
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EFFECT OF CROSS –SECTIONAL SHAPES ON FREE JET CHARACTERIZATION NUMERICAL AND EXPERIMENTAL INVESTIGATION FEASIBLE AND PERFORMANCE OF DIFFERENT EXHAUST GEOMETRY /
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PROPERTIES OF NATURAL POLYMER MATRIX COMPOSITE WITH VARIOUS FIBER ORIENTATIONS /
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A COMPREHENSIVE STUDY OF FLOW THROUGH CIRCULAR PIPE /
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STRUCTURAL ANALYSIS OF AIR CRAFT WINGS WITH VARIOUS CONDITIONS /
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STUDY OF FLIGHT DATA RECORDER SAFETY AND SURVIVAL SYSTEM /
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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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DESIGN AND FABRICATION OF A MICRO UAV WITH DEVELOPMENT OF ITS STRUCTURE, PROPULSION AND CONTROL SYSTEM / Md. Tauhid Rahman Evan, Mir Md. Al Kahman Tamal, Md. Jamal Mian
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DESIGN AND FABRICATION OF AIRFRAME STRUCTURE & CONTROLS OF UAV / Md. Fazlay Robbey, Md. Mukit Hasan, Saiful Islam .
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MEASUREMENT OF DRUG GEOMETRIC MODELS APPLICATION OF FORCE MOMENTUM THEOREM /
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A STUDY OF IMPROVEMENTS ENGINES PERFORMANCE APPLYING INTERCHANGEABILITY ASSOCIATED WITH RAIN AND A NEW APPROACH OF GNESS BASED LANDING SYSTEM /
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GROUND SUPPORT EQUIPMENT OF ‘’ MIST X – 1’’ /
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REVIEW OF OPTICAL FIVER DATA BUS AND FLY- BY LIGHT CONCEPT IN AVIATION /
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DESIGN & MODELING OF RADAR CONTROL SYSTEM FOR DETECTING AIRCRAFT & MISSILE /
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A SCALAR FUNCTION FORMULATION FOR STRESS ANALYSIS OF CYLINDRICAL PANELS /
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ROLE OF COMPOSITES MATERIALS IN AEROSPACE APPLICATIONS – A REVIEW /
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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 AND FABRICATION OF THE FUSELAGE OF A RADIO CONTROLLED AERIAL VEHICLE /
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STUDY MEASUREMENT AND REDUCTION OF RADAR CROSS SECTION (RCS) /
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DESIGN & DEVELOPMENT OF THRUST PROVIDER FOR A HOME BUILT AIRCRAFT (MIST-EXPERIMENTAL-1) /
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STUDY OF GNSS AND ANALYSIS OF ITS IMPROVEMENT FOR POSITIONING ACCURACY /
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DESIGN , CONSTRUCTION AND PERFORMANCE CHECKING OF BLADE ANTENNA /
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DESIGN FEASIBILITY STUDY AND TECHNOLOGY DEMONSTRATION FOR DARAF ,MARKER ,BEACON, AUTO TAXING AND DIGITAL FLIGHT DATA RECORDER /
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COMPARATIVE STUDY OF SWIRL FLOW & JET FLOW /
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COMPARATIVE STUDY OF AIRCRAFT APPROACH AND LANDING PERFORMANCE USING ILS, MLS AND GLS /