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STRESSES IN AN ANGLE PLY LAMINATED CANTILEVER UNDER TRANSVERSE LOADING /
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STRESSES IN AN ANGLE PLY LAMINATED CANTILEVER UNDER SHEAR LOADING / Roohany Mahmud .
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A SCALAR FUNCTION FORMULATION FOR STRESS ANALYSIS OF CYLINDRICAL PANELS /
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DESIGN AND FABRICATION OF AN AUTOPILOT MODEL TO INCORPORATE AUTOMATIC CONTROL OF THE MOMENT OF THE CONTROL SURFACES /
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SCALAR FUNCTION FORMULATION FOR STRESS ANALYSIS OF BOUNDARY VALUE PROBLEMS POLAR AND CYLINDRICAL COORDINATE SYSTEM / Farhan Hasan Nuri, Md. Shoriful Islam .
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PROPERTIES AND MACHINABILITY OF SIC REINFORCED AL-BASED METAL MATRIX COMPOSITE UNDER CNT FLUID / Shafkat Z. Islam, Nawshin Sanjida Haque, Farzana Yeasmin,
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ANALYSIS AND INSTALLATION OF AVIONICS SYSTEM IN A SMALL UNMANNED AIRCRAFT /
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COMPARATIVE ASSESSMENT OF TURBULENCE OF IMPROVED PERFORMANCE OF NAC 0012 AIRFOIL WITH MSBLC /
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DESIGN AND DEVELOPMENT OF A COMBIND TORSION AND BENDING TEST SETUP FOR EVALUATING MECHANICAL PROPERTIES OF MATERIALS /
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DEVELOPMENT OF HYDRAULIC BENDING MACHINE /
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MANUFACTURE AND MISSION PERFORMANCE ANALYSIS OF SMALL UNMANNED AIRCRAFT’ /
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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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INVESTIGATION OF DRAG EFFECT OF AROFOIL SHAPED FUSELAGE UAV MODEL AND VISUALIZATION OF AIR FLOW / Captain Md. Ruhul Amin Noor, Flying Officer Syeda Lira Rayhan & Flying Officer Umme Laila Amin
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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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STUDY OF FLOW CHARACTERISTIC OF A CIRCULAR JET / Umama Sharah Taskia, Maliha Yelmahi, Fatema Tarannum & Afifa Muna.
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STUDY OF FLOW OVER A FANWING IN A SUBSONIC WIND TUNNEL / Sajida Akter Jahan, Sadia Kamal Mery, Tarek Zobaer.
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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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COMPARATIVE STUDY OF SWIRL FLOW & JET FLOW /
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COMPARATIVE STUDY OF AIRCRAFT APPROACH AND LANDING PERFORMANCE USING ILS, MLS AND GLS /
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A COMPARISON OF EXPERIMENTAL WITH SIMULATION EFFECTIVE OF NACA 0012 AIRFOIL WITH BARE /