- #1

vinceguar24

- 1

- 0

- TL;DR Summary
- I'm confused since you need lift to calculate the coefficient and its just a loop.

I'm confused about how to solve for the Cl. I know that the equation for lift is L = Cl * r * .5 * V^2 * A, and you need the Cl to find lift. However the equation for lift coefficient that I found is (2L)/(1/2*p*u^2*S) and you need L which is lift to solve for Cl. So i don't understand how in supposed to solve it. Every website I find doesn't explain it well. it is also the same way for the drag coefficient. If someone would help that would be great. Thanks!!