CONCLUSION


 
 
This project was the occasion for us to get an approach of aeronautics : the two profiles we studied never flied, they are experimental profiles that have been well documented, which allowed us to compare our results with reference results. That was very interesting for us to calculate the lift coefficients and to draw the polar curves, which allow to study the unhooking mecanisms. That was also very interesting to observe how the shock waves are handle by the code: their position on the airfoil, and their thickness. Considering the results we got, we can say that AVBP is doing a good  job.
Usually, bidimensional model give a good idea of the flow over a real 3D airfoil, and they allow to get a first idea for the conception of a new airfoil. But to simulate an entire plane, aeronautics industry uses parallel computation to handle the huge number of simulation points and parameters: we would be proud to do this one day...