I want to find lift per span. What do I have to do? Thank you

Question

I want lift force per span (N/m,rectangular wing) to CFD for strength in solidworks. What should I do? In xflr5 I only see local lift per span. Thank you .

Answer 1

To find the lift force per span in XFLR5, you can go to the "Forces" tab and select "Wing" in the "Associated Areas" dropdown menu. Then you can select "Force per unit span" in the "Distribution" dropdown menu. This will give you the lift force per unit span (N/m) for the entire wing.