Stall control when related to wind turbines is actually the angle of the turbine blade. This angle is adjusted with the direction and speed of the wind.Ê
It has no direct affect on the speed of an object. It does affect the energy content of the speeding object.
It shouldn't affect the speed much, but at different angles (and the same speed), an object can reach different distances.
The weight, aerodynamics, horse power and gear ratios all affect the speed of an automobile.
Temperature, coefficient of restitution, density are some of the factors that affect the speed of sound in a medium.
This varies with the weight of the aircraft, flap positions, weather conditions etc., but the stall speed of your average Boeing 777-200ER with a normal loading of passengers (about 300) on final approach would be around about 140mph.
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.
I am not 100% sure but i think the stall speed of the F-15 eagle is around 500km\h I also saw a documentary that says the stall speed is 530km\h
The stall speed is around 130knots for an F-15 C Eagle
The Auto 5 speed loading feature was introduced in 1954.
164nm
450mph
In landing configuration (full flaps), the stall speed is 40 knots (indicated airspeed). With flaps up it is 48 knots.
The stall speed is classified so it's not publicly available. But it is incredibly low - less than 100 mph.
Typically, an approach is flown at about 15% greater than stall speed. If the target approach speed of the crashed Asiana flight is publiscized at 137 knots, then its stall speed would be about 120 knots (or about 138 mph).
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.
it run down