1 G Stall Tufts Slow Motion
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- Опубліковано 13 вер 2024
- Nominal 1 G stall. Constant chord, constant thickness, no washout low-aspect planform stall characteristics. Stall progresses from aft root rapidly and results in abrupt loss of lift (even in slow motion). Wing tip generates vortex that keeps outboard 2 bays of airflow attached throughout stall, allowing ailerons to remain effective. Airflow rapidly re-attaches with reduction in AOA.
It seems that the UA-cam algorithm just found this one. Excellent demonstration.
yep
It is astonishing that a nearly total flat, smooth surface at high angles creates chaotic vortexs like a jagged surface would
Good video, great example of where and what happens to airflow during a stall. 👍🏼