مواد مشابهة: DESIGN AND CONSTRUCTION OF FLAPPING WING AERIAL VEHICLE (FWAV) /
- STRUCTURAL DESIGN ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE /
- DESIGN AND FABRICATION OF A QUADCOPTER WITH FIXED WING /
- INVESTIGATION OF CAR REAR SPOILER AERODYNAMIC PERFORMANCE USING GURNEY FLAP AT VARIOUS ANGLES ON INVERTED EPPLER 423 /
- PERFORMANCE OPTIMIZATION OF A VARIABLE GEOMETRICAL WING:ANALYSIS AND DESIGN OF MORPHING WING FOR UNMANNED AERIAL VEHICLE /
- DESIGN AND FABRICATION OF A REMOTELY OPERATED UNMANNED COMBAT VEHICLE /
- DESIGN OF A FIXED WING JET PROPULSION POWERED UNMANNED AERIAL VEHICLE (UAV) TARGET DRONE /
موضوع: Mechanical Engineering
- AN EXPERIMENTAL ANALYSIS OF THE THERMAL CONDUCTIVITY AND STABILITY OF CuO-TiO2-ZnO TRIHYBRID NANOFLUID /
- THERMAL BEHAVIOUR OF SN42-BI58 SOLDER ALLOY AND ITS INTERFACIAL CHARACTERISTICS WITH MILD STEEL SUBSTRATES: A SEMI METALLIC BRAKE PAD BACKING PLATE CASE STUDY /
- DEVELOPMENT OF BULLET PROTECTIVE PANEL FROM RECYCLED TIRES /
- DESIGN AND DEVELOPMENT OF A NOVEL BIODEISEL PROCESSOR AND PERFORMANCE ANALYSIS OF B1OO BIO DIESEL PRODUCED FROM SOYBEAN OIL / Md.Shihab Uddin, Sarjil Mehedi, M A.Masum Bulbul Chowdhwary.
- DESIGN AND FABRICATION OF A VAPOR ABSORPTION REFRIGERATION SYSTEM / Mosharrouf Hossain, S.M Rafid Rahman, Saadman Shoumik.
- STUDY OF SMALL AND MEDIUM ENTERPRISES (SME) PRODUCTS IN BANGLADESH: PERFORMANCE AND QUALITY IMPROVEMENT OF A SELECTED PRODUCT / Muksadur Rahman, Md Nazrul Huda Aslam, Jakia sultana.
موضوع: This Thesis Paper of ME in BSc Program.
- AN EXPERIMENTAL ANALYSIS OF THE THERMAL CONDUCTIVITY AND STABILITY OF CuO-TiO2-ZnO TRIHYBRID NANOFLUID /
- THERMAL BEHAVIOUR OF SN42-BI58 SOLDER ALLOY AND ITS INTERFACIAL CHARACTERISTICS WITH MILD STEEL SUBSTRATES: A SEMI METALLIC BRAKE PAD BACKING PLATE CASE STUDY /
- DEVELOPMENT OF BULLET PROTECTIVE PANEL FROM RECYCLED TIRES /
- DESIGN AND CONSTRUCTION OF FLAPPING WING AERIAL VEHICLE (FWAV) /
- SYNERGISTIC FLOW CONTROL: INGRATION OF DYNAMIC VORTEX GENERATORS AND VARYING DIMPLE GEOMETRIES FOR ENHANCED AERODYNAMIC CHARACTERISTICS FOR NACA 2412 AIRFOIL /
- OPTIMIZATION AND PREDICTION OF THE MACHINABILITY OF HEAT-TREATED ALUMINUM COMPOSITE USING A DATA-DRIVEN APPROACH AND SUBSEQUENT EXPERIMENTAL VALIDATION /