Flow simulation over NACA airfoil

Flow Simulation over a NACA airfoil is carried out at a velocity of 600m/s in x-direction, for different angle of attack, viz. 0,2,4,6,8 and 10.

In the following model, only 0 degree angle of attack is shown(but for results it was changed over and over again).

https://drive.google.com/file/d/11rI_5kAaZtmLemt56M0zAcReNxOLuJ8w/view?usp=sharing

Comparision between lift force(force in y-direction) and drag force(force in x-direction) is shown for angle of attack:

0

https://drive.google.com/file/d/107Sh7AI_Rly9n3MogTWCVAhIGoMqdtuO/view?usp=sharing

https://drive.google.com/file/d/1SMo59Sr_iPZFWBjYEkOxnaQEmfTvWO_q/view?usp=sharing

2

https://drive.google.com/file/d/1o6j2Klb8zIRtfe8kymrso3U9HkiDomE6/view?usp=sharing

https://drive.google.com/file/d/1JBeZINRfSRoHk0u1A4DJ7-Jy09DoilGh/view?usp=sharing

4

https://drive.google.com/file/d/1AEfDwFHc9t5MK_UHdSq5wn-gVt5Kq3Ls/view?usp=sharing

https://drive.google.com/file/d/1TlgdhqDhyxVdQ38CG2WIzx3Yu9CzkSo4/view?usp=sharing

6

https://drive.google.com/file/d/1Ty_CgszLlHMKb7Micombmcw1Tz3hsy7w/view?usp=sharing

https://drive.google.com/file/d/1uaPgzyYrUxBquR0zc2NDnJyOyDzR_Yi3/view?usp=sharing

8

https://drive.google.com/file/d/1rUhAesFsLjyh9IuKukzPMA8z13k4OaQJ/view?usp=sharing

https://drive.google.com/file/d/1hNypcvu90_KtTfVSjoii0Vtjx72i6I7W/view?usp=sharing

10

https://drive.google.com/file/d/1J7r5cDb_y4m9KkIYBCotd2t9BlSbSecK/view?usp=sharing

https://drive.google.com/file/d/1O2bOiDJZg64fg58JDGuyupsWgsOEO9OS/view?usp=sharing