![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/Uyd8D.jpg)
aircraft design - Why doesn't the minimum drag point meet the point at the best Cl/CD polar? - Aviation Stack Exchange
![Example of a drag polar for a cambered wing. Notice that the difference... | Download Scientific Diagram Example of a drag polar for a cambered wing. Notice that the difference... | Download Scientific Diagram](https://www.researchgate.net/publication/236669766/figure/fig7/AS:299541829046279@1448427745565/Example-of-a-drag-polar-for-a-cambered-wing-Notice-that-the-difference-between-C-D0-and.png)
Example of a drag polar for a cambered wing. Notice that the difference... | Download Scientific Diagram
![Estimating aircraft drag polar using open flight surveillance data and a stochastic total energy model - ScienceDirect Estimating aircraft drag polar using open flight surveillance data and a stochastic total energy model - ScienceDirect](https://ars.els-cdn.com/content/image/1-s2.0-S0968090X19307764-gr9.jpg)
Estimating aircraft drag polar using open flight surveillance data and a stochastic total energy model - ScienceDirect
![Direct Calculation of Zero-Lift Drag Coefficients and (L/D)max in Subsonic Cruise | Journal of Aircraft Direct Calculation of Zero-Lift Drag Coefficients and (L/D)max in Subsonic Cruise | Journal of Aircraft](https://arc.aiaa.org/cms/10.2514/1.C035717/asset/images/medium/figure3.gif)