# How to get Lift and drag coefficient for an airfoil

**URL:** https://discourse.paraview.org/t/how-to-get-lift-and-drag-coefficient-for-an-airfoil/14652
**Category:** ParaView Support
**Created:** [May 17, 2024, 8:27am UTC](https://discourse.paraview.org/t/how-to-get-lift-and-drag-coefficient-for-an-airfoil/14652 "2024-05-17T08:27:08Z")
**Posts on this page:** 1
**Page:** 1

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### Author: ![Kamal\_Ihsan\_Kamarudd](https://discourse.paraview.org/user_avatar/discourse.paraview.org/kamal_ihsan_kamarudd/32/13265_2.png) [@Kamal\_Ihsan\_Kamarudd](https://discourse.paraview.org/u/Kamal_Ihsan_Kamarudd)
#### Post date: [May 17, 2024, 8:27am UTC](https://discourse.paraview.org/t/how-to-get-lift-and-drag-coefficient-for-an-airfoil/14652/1 "2024-05-17T08:27:09Z")

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Can you guys show me step by step how to get lift and drag coefficient for an airfoil