Journal of Energy Systems Theoretical and computational studies on the optimal positions of NACA airfoils used in horizontal axi
![In the Cl vs Cd graph, Why the drag coefficient decreases initially with the small increment in lift coefficient? - Aviation Stack Exchange In the Cl vs Cd graph, Why the drag coefficient decreases initially with the small increment in lift coefficient? - Aviation Stack Exchange](https://i.stack.imgur.com/qsxQF.png)
In the Cl vs Cd graph, Why the drag coefficient decreases initially with the small increment in lift coefficient? - Aviation Stack Exchange
![aircraft design - Why doesn't the minimum drag point meet the point at the best Cl/CD polar? - Aviation Stack Exchange aircraft design - Why doesn't the minimum drag point meet the point at the best Cl/CD polar? - Aviation Stack Exchange](https://i.stack.imgur.com/HnFGy.jpg)