AERODYNAMICS BASED PROJECT AD01 Control of flow through airfoils by the use of dimples of varying shapes AD02 Experimental investigation and analysis of the flow field through the blunt fin with the dimples AD03 The dimpled surface of a spherical has certain aerodynamic characteristics and flow patterns. AD04 The hang-glider that was designed by Angelo Darrigo was given several winglets in order to increase its turning and soaring capabilities. AD05 A numerical analysis of the effectiveness of wing boundary layer management in reducing wingtip shed vortices AD06 Simulation of aircraft flight using numerical flow data AD07 An investigation into the enhancement of the top surfaces of airfoil sections using various flow visualisation methods AD08 Research into a high-performance co-flow jet airfoil, both experimental and computational in nature AD09 Modelling of aerodynamic zero-lift drag and its application in adapt AD10 Using overset meshing, a CFD study was performed on the main rotor blade of a scale model helicopter. AD11 Research on the effectiveness of various airfoils used to the outer parts of big rotor blades AD12 An examination of the behaviour of foils and wings when the Reynolds number is low AD13 A computational investigation of the flying aerodynamic system, focusing on the flap. AD14 Analysis of the aeroelastic behaviour of aircraft complete with control surfaces using CFD AD15 Effect that winglets have on a jet transport wing of the first generation AD16 An investigation of the effects of aerodynamic drag on the deployment of multiple winglets on light aircraft AD17 Comparison of the aerodynamic performance of an aeroplane wing model with and without a winglet resembling bird feathers AD18 An investigation on the aircraft configuration known as blended wings and bodies. AD19 Eliminating excess air resistance with an aircraft model by using an elliptical winglet AD20 An inquiry of the effects of using several winglets via experimentation AD21 Analysis of the aerodynamic effects of many winglets on slow-moving aircraft AD22 An investigation on the effects of contemporary spiroid winglets on the aerodynamic performance of a swept-wing model was carried out. AD23 Analytical and experimental research of the aerodynamics of wingtip sails using three different types of winglets AD24 Analysis of the flying characteristics of a wing having numerous winglets AD25 Analysis of winglets using CFD at low subsonic flow conditions AD26 The development of winglets for aeroplanes travelling at low speeds Read More >>
