Extra weight (for example, carrying more cargo) increases the stalling speed, and a lower weight (e.g. minimum fuel) reduces it.
The stalling speed increases when 'pulling G' because the lift required to support the increased weight of the aircraft at higher G-forces also increases. This higher lift requirement means the aircraft needs to maintain a higher speed to prevent stalling.
It increases.
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.
Drag increases by the square of velocity increase, for example, tripling speed increases drag by a factor of nine!
Depends on the airplane. A small Cessna might have a minimum speed of 40 mph, while a large passenger aircraft might have a minimum speed of 150mph or more. The actual speed for a given airplane will vary based on weight and flap configuration.
Assuming it as passenger aircraft and take-off speed = lift off speedwe have minimum runway length required as 80*35 = 2.8kmIf it is a military aircraft the length will reduce further to minimum unstick speed
The minimum speed of a Boeing 767 to remain in flight is about 160 miles per hour. Anything below that will cause the aircraft to begin to stall.
By adding thrust to the engine or pitching downwards
Unfortunately, this is much too general to answer. It completely depends on the type, manufacturer, and model of the aircraft.
Aircraft speed and altitude cannot alter air pressure and how it complies with Bernoulli's principle. Aircraft speed decreases the pressure on the wings of the aircraft but this does not alter air pressure.
Most aircraft have different landing angels dependent on weight, wing shape and stalling speed.