Samankaltaisia teoksia: PROPULSION SYSTEM OF A TARGET DRONE /
- DESIGN AND FABRICATION OF A TARGET DRONE /
- DESIGN OF A FIXED WING JET PROPULSION POWERED UNMANNED AERIAL VEHICLE (UAV) TARGET DRONE /
- STABILITY AND PERFORMANCE ANALYSIS OF A FIXED WING (UNMANNED AERIAL VEHICLE) TARGET DRONE FOR TESTING AND AIR DEFENCE SYSTEM TARGET DRONE /
- STRUCTURAL DESIGN OF A TARGET DRONE /
- DESIGN AND DEVELOPMENT OF TARGET DRONE: STABILITY AND CONTROL ANALYSIS /
- DESIGN AND DEVELOPMENT OF FUEL SYSTEM & LANDING GEAR FOR TARGET DRONE /
Aihe: Aeronautical Engineering
- COMPARATIVE STUDY OF SWIRL FLOW & JET FLOW /
- COMPARATIVE STUDY OF AIRCRAFT APPROACH AND LANDING PERFORMANCE USING ILS, MLS AND GLS /
- MANUFACTURE AND MISSION PERFORMANCE ANALYSIS OF SMALL UNMANNED AIRCRAFT’ /
- A COMPARISON OF EXPERIMENTAL WITH SIMULATION EFFECTIVE OF NACA 0012 AIRFOIL WITH BARE /
- EFFECT OF CROSS –SECTIONAL SHAPES ON FREE JET CHARACTERIZATION NUMERICAL AND EXPERIMENTAL INVESTIGATION FEASIBLE AND PERFORMANCE OF DIFFERENT EXHAUST GEOMETRY /
- PROPERTIES OF NATURAL POLYMER MATRIX COMPOSITE WITH VARIOUS FIBER ORIENTATIONS /
Aihe: This Thesis Paper of AE in B.Sc. Program.
- DESIGN, ANALYSIS AND OPTIMIZATION OF A SMALL UNMANNED AIRCRAFT /
- ANALYSIS OF DESIGN FLAWS IN AN UNMANNED AERIAL VEHICLE (UAV) TARGET DRONE AND FABRICATION, CFD ANALYSIS AND TUNNEL TESTING OF A 3D MODEL POST AMENDMENT /
- DESIGN AND FABRICATION OF A TARGET DRONE /
- SHAPE OPTIMIZATION OF GURNEY FLAP ON AIRFOIL /
- FABRICATION OF AL-6063 METAL MATRIX HYBRID COMPOSITE REINFORCED WITH SIC NANOPARTICALS BY STRI CASTING /
- DESIGN & DEVELOPMENT OF A SOFTWARE TOOL FOR ANALYSIS OF THE CHARACTERISTICS OF INSTRUMENTED RECTILINEAR OPEN LOOP CONTROL SYSTEM /
Tekijä: Saleh, Sheikh Ahmed Abu
Tekijä: Sobhan, Rehman
- Collected Works of Rehman Sobhan : Milestones to Bangladesh Vol-2 /
- Collected Works of Rehman Sobhan : Challenging InjusticeThe Odyssey of a Bangladeshi Economist Vol-1 /
- Collected Works of Rehman Sobhan : The Political Economy of Malgovernance Bangladesh Vol-3 /
- PROPULSION SYSTEM OF A TARGET DRONE /