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STRESSES IN AN ANGLE PLY LAMINATED CANTILEVER UNDER SHEAR LOADING / Roohany Mahmud .
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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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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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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 COMPREHENSIVE STUDY OF FLOW THROUGH CIRCULAR PIPE /
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EFFECTIVENESS AND DESIGN OF SHEAR WALL STRUCTURE UNDER LATERAL LOAD /
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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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DESIGN & MODELING OF RADAR CONTROL SYSTEM FOR DETECTING AIRCRAFT & MISSILE /
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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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PROPERTIES OF NATURAL POLYMER MATRIX COMPOSITE WITH VARIOUS FIBER ORIENTATIONS /
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MODELING AND SIMULATION OF LONGITUDINAL AUTOPILOT FOR GENERAL AVIATION AIRCRAFT /
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STRUCTURAL ANALYSIS OF AIR CRAFT WINGS WITH VARIOUS CONDITIONS /
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STUDY AND DESIGNING OF MICRO CONTROLLER BASED TEMPERATURE SENSING SYSTEM ALONG WITH GLOBAL SYSTEM FOR MOBILE INTERFACE AND ALARM MECHANISM TO BE USED IN EFFERENT TEMPERATURE SENSITIVE STOREHOUSES /
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STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY LAYER CONTROL ( MSBC) ON SINGLE & DOUBLE CYLINDER CONFIGURATION NACA 23018 AIRFOIL /
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LARGE DEFECTION ANALYSIS OF AN AIRCRAFT WING WITH ELLIPTICAL LIFT DISTRIBUTION AT DIFFERENT FLIGHT CONDITION /
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DETECTION OF OBJECTS IN 2-D USING SONAR SENSOR /
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CONSTRUCTION AND STUDY OF VALUELESS PURSUIT ENGINE /
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STUDENT ANALYSIS OF AIRCRAFT WINGS WITH VARIOUS CONDITIONS /
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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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SHEET MOLDING COMPOUND (SMC) FROM CARBON NANO PARTICLE / Md. Rafid Washir, Morshed Mahmud, Md. Khayrul Islam Shakil.
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EFFECT OF ROTATING CYLINDER ON THE PERFORMANCE OF SYMMETRIC AIRFOIL: “AN EXPERIMENTAL STUDY /