![aircraft design - Does an airfoil drag coefficient takes parasite drag into account? - Aviation Stack Exchange aircraft design - Does an airfoil drag coefficient takes parasite drag into account? - Aviation Stack Exchange](https://i.stack.imgur.com/jQlcj.png)
aircraft design - Does an airfoil drag coefficient takes parasite drag into account? - Aviation Stack Exchange
Solved] In the figure below you see the hypothetical lift-drag polar of an aircraft Q1: For this aircraft, determine the maximum glide ratio ? | Course Hero
![Comparison of aerodynamic analysis drag polar curve prediction with... | Download Scientific Diagram Comparison of aerodynamic analysis drag polar curve prediction with... | Download Scientific Diagram](https://www.researchgate.net/publication/262185433/figure/fig6/AS:667663751712785@1536194851620/Comparison-of-aerodynamic-analysis-drag-polar-curve-prediction-with-wind-tunnel-test.png)
Comparison of aerodynamic analysis drag polar curve prediction with... | Download Scientific Diagram
![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
![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)