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
A stall occurs when the flow of air over an aircraft’s wings is disrupted, causing a loss of lift and control. Pilots are trained to recognize and recover from stalls by reducing the aircraft’s angle of attack to regain lift and control.
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.
The stall speed of the Airbus A340-200 typically ranges from about 105 to 115 knots, depending on factors such as aircraft weight, configuration, and environmental conditions. Stall speed is the minimum speed at which an aircraft can maintain level flight and varies based on these variables. For precise values, refer to the aircraft's specific operating manual or performance data.
A sudden and potentially dangerous loss of lift in an aircraft is known as a stall. This occurs when the angle of attack is too high, causing the airflow over the wings to become disrupted and the aircraft to lose its ability to generate lift. It can lead to a loss of control and potential stalling of the aircraft.
Yes, increasing the weight or load of an aircraft will increase its stall speed. This is because more lift is required to support the extra weight, which means the aircraft must be moving faster to generate that lift and avoid stalling.
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 stall speed of the MiG-29K, a carrier-based multirole fighter aircraft, is approximately 130 to 140 knots (about 150 to 160 mph or 240 to 260 km/h) depending on various factors such as weight, configuration, and environmental conditions. Stall speed can vary based on the aircraft's load and specific flight configurations. For accurate and specific data, consult the aircraft's technical manuals or manufacturer specifications.