Những quyển sách tương tự: 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 /
Đề tài: Mechanical Engineering
- PRESERVATION OF MEDICINES & VACCINES BY THERMOMETRIC (PELETIER) REFRIGERATION UNIT IN BANGLADESH PERSPECTIVE /
- A COMPREHENSIVE ANALYSIS & CONSTRUCTION OF RENEWABLE MICRO HYDRO POWER GENERATION PROJECT /
- DESIGN AND CONSTRUCTION OF A FLAT PLATE ABSORBER SOLAR WATER HEATER /
- STUDY OF FLOW THROUGH A CIRCULAR PIPE AND CONSTRUCTION OF AN EXPERIMENTAL SET UP FOR THE STUDY /
- DESIGNING & MANUFACTURING OF A PUNCHING SHEAR ASSEMBLY BLOCK & CUTTERS) AS PERT OF DIRECT SHEAR TEST SETUP /
- EXPERIMENTAL STUDY ON THE PERFORMANCE OF MEDICAL INDUCED DRAFT COOKING TOWER USING DIFFERENT QUALITY OF CIRCULATING FLUIDS /
Đề tài: This Thesis Paper of ME in BSc Program.
- NUMERICAL INVESTIGATION OF CONVECTIVE HEAT TRANSFER FOR TURBULENT FLOW IN A PERIODICALLY SEMI-ELLIPTICAL GROOVED TUBE USING HYBRID NANOFLUIDS /
- THERMAL - HYDRAULIC PERFORMANCE ENHANCEMENT WITH MINIMUM ENTROPY GENERATION OF A HEAT EXCHANGER USING QUADCOPTER FRAME VORTEX GENERATOR /
- PERFORMANCE TEST OF AN REFRIGERATION SYSTEMS EVAPORATOR SECTION WITH HEAT PIPE /
- DAMAGE CHARACTERIZATION OF GLASS FIBRE REINFORCED POLYMER (GFRP) COMPOSITES /
- MECHANICAL PERFORMANCE OF HYBRID GRAPHENE- BASALT FIBER COMPOSITES FOR LIGHTWEIGHT SPAR CAP APPLICATIONS IN WIND TURBINES /
- INVESTIGATION OF PARAMETRIC SURFACE CAVITIES ON THE TRANSONIC AERODYNAMIC PERFORMANCE OF THE RAE 2822 AIRFOIL /