Ítems similars: DEVELOP A CUT VIEW MODEL OF JET ENGINE /
- ACTIVE CONTROL OF FLOW SEPARATION OVER SUPERCRITICAL AIRFOIL USING SYNTHETIC JET /
- STUDY OF IMPACT OF JET ON DIFFERENT VANES FOR MEASURING FLOW RATE AND IMPACT FORCE /
- DESIGN AND DEVELOPMENT OF A MULTI BARREL PROJECTILE LAUNCH SYSTEM /
- DESIGN AND DEVELOPMENT OF A CONTROL SYSTEM FOR SELF BALANCINGTWO WHEELER ROBOT /
- SUSTAINABLE ENERGY SOLUTION FOR REMOTE AREAS : A PICO HYDROPOWER MODEL FOR HILLY REGIONS OF BANGLADESH /
- DESIGN AND FABRICATION OF A REMOTELY OPERATED UNMANNED COMBAT VEHICLE /
Tema: Mechanical Engineering
- 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 /
- DESIGN AND PERFORMANCE ANALYSIS OF AN ENHANCED SUBMERGED EVAPORATOR FOR MID-RANGE (5-10) AIR COOLED CHILLER SYSTEMS /
- SUSTAINABLE ENERGY SOLUTION FOR REMOTE AREAS : A PICO HYDROPOWER MODEL FOR HILLY REGIONS OF BANGLADESH /
- DESIGN , OPTIMIZATION AND PERFORMANCE EVALUATION OF A SOLAR HEAT COLLECTOR TROUGH AUTOMATED DATA ACQUISITION SYSTEM / Nashid Ibne Shahid, Mustahseen Indaleeb, Dewan Akramul Haque .
Tema: This Thesis Paper of ME in B.Sc. Program.
- DEVELOP A CUT VIEW MODEL OF JET ENGINE /
- STRUCTURAL DESIGN ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE /
- DETERMINATION OF CRITICAL SPEED OF A SHAFT /
- DESIGN AND FABRICATION OF MODEL SURFACE TO SURFACE MISSILE LAUNCHING SYSTEM /
- DESIGN AND FABRICATION OF A MODEL SURFACE TO SURFACE MISSILE WITH MOTION CONTROL SYSTEM RUN BY COST-EFFECTIVE SOLID PROPELLANT /
- DESIGN AND FABRICATION OF A REMOTELY OPERATED UNMANNED COMBAT VEHICLE /