![aircraft design - How do you calculate the lift coefficient of an airfoil at zero angle of attack? - Aviation Stack Exchange aircraft design - How do you calculate the lift coefficient of an airfoil at zero angle of attack? - Aviation Stack Exchange](https://i.stack.imgur.com/SqspU.jpg)
aircraft design - How do you calculate the lift coefficient of an airfoil at zero angle of attack? - Aviation Stack Exchange
![Will this simple equation (pic attached) produce a rough estimate of the top speed of a prop driven aircraft? - Aviation Stack Exchange Will this simple equation (pic attached) produce a rough estimate of the top speed of a prop driven aircraft? - Aviation Stack Exchange](https://i.stack.imgur.com/Oaxzj.gif)
Will this simple equation (pic attached) produce a rough estimate of the top speed of a prop driven aircraft? - Aviation Stack Exchange
![Lift coefficient plotted as a function of angle of attack (schematic). | Download Scientific Diagram Lift coefficient plotted as a function of angle of attack (schematic). | Download Scientific Diagram](https://www.researchgate.net/publication/2611242/figure/fig1/AS:669528954523663@1536639550828/Lift-coefficient-plotted-as-a-function-of-angle-of-attack-schematic.png)
Lift coefficient plotted as a function of angle of attack (schematic). | Download Scientific Diagram
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