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
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