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Slats are used to reconfigure the wing in a high speed, or high angle-of-attack maneuover. When the units of angle of attack increase, the wing chord decreases. Slats compensate for this occurance.
Extra weight (for example, carrying more cargo) increases the stalling speed, and a lower weight (e.g. minimum fuel) reduces it.
Most aircraft have different landing angels dependent on weight, wing shape and stalling speed.
velocity diagram indicate the effect of vane angle, effect of jet angle on impeller speed
Yes plus speed
wings with smaller aspect ratio stall at higher angle of attack .. and wings with larger aspect ratio stall at a lower angle of attack ... stall can take place at any air speed but only a specific angle of attack.. my view says aspect ratio has no relation to stall speed.
A: The pitch angle is a speed factor and also a torque factor. Increasing or decreasing the angle will effect these factors inversely
Slats and flaps increase drag and also increaselift. The increase in drag slows the aircraft down, and the increase in lift lowers the stall speed, which slows the landing speed of the aircraft.
Stalling.
It has a top speed limiter. Once you reach that speed it will shut the engine off
Velocity is speed in a direction or speed at an angle. The velocity changes when the speed or angle changes.
It could be a clogged fuel filter.