The stalling of an aircraft wing is caused by the disruption of the airflow on the upper and lower surfaces of the wing, An airflow is travelling fast enough over a wing. A low pressure area develops on the underside of the wing and a very high pressure on the upper surface of the wing ......This is what causes lift- the force that allows the aircraft to fly. If this airflow is Broken or reaches a speed too slow to maintain the low pressure required to create the lift. The wing will stall
That would be a wing stall, or just, 'stall'. This kind of stall has nothing to do with the aircraft's engine, if it has one.
Stall
Answer 1As an airplane's wing moves through the air, the faster moving air on the top of the wing creates a low pressure zone or "lift" which keeps the airplane up and flying. If anything happens to deflect or destroy that proper airflow (smooth flow of air around the wing) the wing loses lift, and is said to stall.This could be from loss of speed or too much angle of attack (pulling back to hard)In many cases the actual stall is preceded by a buffet (shaking) In Many cases you can avoid the stall by lowering the nose of the aircraft.A spin is an aggravated stallYes that is true but another reason an aircraft could stall is because the service celing of the aircraft has been reached the aircraft can no longer produce enough thrust to keep it in the air because the air is too thin or the engines aren't strong enough
The stall speed of an aircraft depends on its altitude, weight, configuration, and lateral and vertical acceleration. The stall speed for a 777 is dependent on these real-time factors.
A Clean Stall is happens in the aircrafts normal cruise configuration. A Dirty Stall is occurs in the landing configuration, landing gear, slats, flaps in the landing position.
probably a stall, but they are not that dangerous, if you are trained to get out of them
Airbus aircraft do not use stall vanes for stall warning. Airbus use a sophisticated system of stall prevention instead, with the angle of attack and slat settings are primary parameters in the fly-by-wire computer system.The angle of attack is determined by two electrically heated alpha probes on either side of the forward fuselage.As the aircraft approaches a stall condition, (in normal law) the flight computers take control and return controls to a non-stall position.
A 1998 Honda Accord could stall because it is out of gas. The car could also stall because of a bad computer.
The smoke and ash in the air can either blind the pilot or stall the engine
sensor or belt
sensor or belt
Almost any aircraft egine will stall if ingesting ash instead of clean air. Clean air is essential to an engine's performance