airfoil - What is the effect of flow separation on lift, pressure
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Consider an airfoil (a wing) in an airflow. When angle of attack increases, at some point the flow start to separate from trailing edge. By increasing the angle of attack more, this separation area
![](https://ars.els-cdn.com/content/image/1-s2.0-S1000936113001295-gr4.jpg)
Numerical study of separation on the trailing edge of a symmetrical airfoil at a low Reynolds number - ScienceDirect
![](https://www.researchgate.net/publication/305719086/figure/fig1/AS:786278320726017@1564474768306/Flow-Separation-and-Profile-Drag-on-an-Airfoil.png)
Flow Separation and Profile Drag on an Airfoil.
![](https://web.mit.edu/2.972/www/reports/airfoil/airfoil-2.gif)
2.972 How An Airfoil Works
Aerodynamics vs pressure Gradient
![](https://www.egr.msu.edu/tmual/CHuck/static_12deg.gif)
Dynamic Stall Research
![](https://eaglepubs.erau.edu/app/uploads/sites/4/2021/08/Airfoil_LiftFlap-1024x860.png)
Aerodynamics of Airfoil Sections – Introduction to Aerospace
![](https://eaglepubs.erau.edu/app/uploads/sites/4/2021/08/Airfoil_TEseparation.png)
Stalling & Spinning – Introduction to Aerospace Flight Vehicles
![](http://ffden-2.phys.uaf.edu/211.fall2000.web.projects/c.%20Schaefer/aero4_files/image001.gif)
Paper Airfoil Aerodynamics
![](https://i.stack.imgur.com/hOwvq.png)
airfoil - What is the effect of flow separation on lift, pressure distribution and drag? - Aviation Stack Exchange