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.
The stall speed of an airplane is inversely proportional to the square root of the load factor. Therefore, with a load factor of 4, the stall speed would be 35 knots (70 knots / √4).
The stall speed of a Boeing 747 heavy (747-400 or -8 model) is around 155-165 knots indicated airspeed (KIAS) at typical landing weight. This speed can vary based on factors such as weight, configuration, and atmospheric conditions.
Weight affects lift because as an object gets heavier, it requires more lift force to counteract gravity and stay airborne. This means that a heavier object will need more thrust or a larger wing surface area to generate enough lift to support its weight. Additionally, weight can impact the wing loading and stall speed of an aircraft.
To increase the speed of displaying pictures in your app, consider reducing the image resolution, optimizing image loading processes, implementing lazy loading techniques, and using caching mechanisms to store and retrieve images more efficiently. Additionally, consider preloading images that will be displayed soon to reduce loading times.
Stall control in wind turbines involves adjusting the angle of the turbine blades to maintain optimal performance. When wind speeds increase, the blades are pitched to "stall" or reduce their lift, preventing damage and providing a safeguard in high winds. This control method helps to regulate the turbine's speed and prevent potential overload.
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 of an airplane is inversely proportional to the square root of the load factor. Therefore, with a load factor of 4, the stall speed would be 35 knots (70 knots / √4).
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.