CFD OF SMALL GLIDER (STRUCTURAL AND AERODYNAMIC ANALYSIS)

A glider needs to be simulated. The velocity contours and pressure contours of the full glider, pressure contours of the wing at different angles. A tip deflection structural analysis of the wing itself. This is bending stress to find at what bending distance the wing will break using a 5kg load at the tip. The speed is 3/ms the angles are 0,2,4,6,8,10. cl and cd required at all these angles. I require this by 9pm 29th May at the latest. Project will be awarded at 8am 29th may. This is not a complex difficult job, the glider is 2.1m wide and 2m long. It is made in solidworks. Ansys to be used for cl and cd Solidworks if you need for the rest. Lowest price gets the job.