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STRESSES IN AN ANGLE PLY LAMINATED CANTILEVER UNDER TRANSVERSE LOADING /
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STRESSES IN ANGEL PLAY LAMINATED CANTILEVER UNDER BENDING MOMENT /
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A SCALAR FUNCTION FORMULATION FOR STRESS ANALYSIS OF CYLINDRICAL PANELS /
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EFFECTIVENESS AND DESIGN OF SHEAR WALL STRUCTURE UNDER LATERAL LOAD /
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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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DESIGN AND IMPLEMENTATION OF A LAW COST ATTITUDE HEADING REFERENCE SYSTEM FOR LAW SPEED AIRCRAFT / Md. Shajid-Ul-Mahmud, Tariqul Islam, Md. Saiful Islam,
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ELECTROTHERMAL BEHAVIOR OF ANGLED FIBER-REINFORCED COMPOSITE LINES /
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PERFORMANCE ANALYSIS OF FIXED AND MORPHING WINGS USING NACA 4412 ASYMMETRIC AIRFOILS UNDER VARYING ANGLES OF ATTACK AND FLOW REGIMES /
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A STUDY ON MULTIPLICATION DISPLAY AND SIMULATION OF MFD SYMBOLOGY /
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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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BEHAVIOR AND EFFECTIVENESS OF SHEAR WALL STRUCTURE UNDER LATERAL LOAD /
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SHEET MOLDING COMPOUND (SMC) FROM CARBON NANO PARTICLE / Md. Rafid Washir, Morshed Mahmud, Md. Khayrul Islam Shakil.
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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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MANUFACTURE AND MISSION PERFORMANCE ANALYSIS OF SMALL UNMANNED AIRCRAFT’ /
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ANALYSIS AND INSTALLATION OF AVIONICS SYSTEM IN A SMALL UNMANNED AIRCRAFT /
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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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STUDY OF FLOW CHARACTERISTIC OF A CIRCULAR JET / Umama Sharah Taskia, Maliha Yelmahi, Fatema Tarannum & Afifa Muna.
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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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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 .