Gelijkaardige items: EXPERIMENTAL STUDY ON THE EFFECT OF DIFFERENT WINGLET CONFIGURATIONS ON THE LIFT AND DRAG CHARACTERISTICS OF A BLENDED WING BODY AIRCRAFT /
- EXPERIMENTAL STUDY ON THE EFFECT OF DIFFERENT WINGLET CONFIGURATIONS ON THE LIFT AND DRAG CHARACTERISTICS OF A BLENDED WING BODY AIRCRAFT
- ANALYSIS OF AERODYNAMIC PERFORMANCE OF BLENDED WING BODY WITH VORTEX GENERATORS AND WINGLETS /
- EXPERIMENTAL STUDY OF FLOW CHARACTERISTICS AROUND DIFFERENT SHAPED BODIES AND TO FIND THE RESULTING DRAG /
- "INFLUENCE OF SURFACE MODIFICATION ON THE LIFT-DRAG CHARACTERISTICS OF NACA 0012 AIRFOIL" /
- LARGE DEFECTION ANALYSIS OF AN AIRCRAFT WING WITH ELLIPTICAL LIFT DISTRIBUTION AT DIFFERENT FLIGHT CONDITION /
- DEVELOPMENT OF A CFD MODEL FOR SIMULATING THE AERODYNAMIC PERFORMANCE OF A BLENDED WING BODY AIRCRAFT (WITH AND WITHOUT VORTEX GENERATOR) /
Onderwerp: 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 /
Onderwerp: 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 /