Simulation of the air flow through the wing using ANSYS (fluent) 19.1

In this tutorial i just show you how to see the model of the airflow passing through the wing at the maximum AOA (Angle of Attack) using ANSYS Fluent at the last Steps (Result).
Dont Forget to LIKE and SUBSCRIBE this Video..
the link of the other steps using ANSYS fluent that you may wanna look at :
- • how to calculate lift ...
- • how to calculate lift ...

[@brudhelbamokila7682]

Hello,
Thanks for this video. I am studying the flow around a 3D wing and would like help with the reference values ​​to be specified in Ansys Fluent. I know the area is the top surface of the wing, the length is that of the chord. But my problem is that the chord is not constant all the way down the wing (the chord at the root is bigger than the salmon one). How can I specify the chord in this case, please ?

[@pjok020lb5]

Thanks mr.arjen...🙏

[@arjenalves2204]

hahah sama-sama wong_gamers