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In fluid dynamics, a stall is a reduction in the lift coefficient generated by a foil as angle of attack exceeds its critical value. The critical angle of attack is typically about 15°, but it may vary significantly depending on the fluid, foil – including its shape, size, and finish – and Reynolds number.
History, Types & In accelerated and turning flight
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stall aircraft angle attack wing lift speed flight deep critical may also airspeed stalls stalling flow pilot wings higher control
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| severe turbulence | instance of | or from less likely sources | 0.80 | text |
| a stick shaker | instance of | If pre-stall warning followed by nose drop and limited wing drop are naturally not present or are deemed to be unacceptably marginal by an Airworthiness authority the stalling b… | 0.80 | text |
| pusher | instance of | If pre-stall warning followed by nose drop and limited wing drop are naturally not present or are deemed to be unacceptably marginal by an Airworthiness authority the stalling b… | 0.80 | text |
| a Mitsubishi MU-2 is flying close to its stall speed | instance of | When an aircraft | 0.80 | text |
| the sudden application of full power may cause it to roll | instance of | When an aircraft | 0.80 | text |
| creating the same aerodynamic conditions that induce an accelerated stall in turning flight even if the pilot did not deliberately initiate a turn | instance of | When an aircraft | 0.80 | text |
| a fence | instance of | The amount of boundary layer air flowing outboard can be reduced by generating vortices with a leading-edge device | 0.80 | text |
| notch | instance of | The amount of boundary layer air flowing outboard can be reduced by generating vortices with a leading-edge device | 0.80 | text |
| saw tooth or a set of vortex generators behind the leading edge | instance of | The amount of boundary layer air flowing outboard can be reduced by generating vortices with a leading-edge device | 0.80 | text |
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