Stall Speed vs. Weight and Altitude

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Stall speed increases with aircraft weight because a heavier aircraft requires more lift, necessitating a higher speed to maintain the same maximum coefficient of lift (CLmax). Additionally, stall speed is affected by altitude due to changes in air density; as altitude increases, air density decreases, requiring a faster speed to generate the same lift. Therefore, both increased weight and higher altitude lead to higher stall speeds. Understanding these relationships is crucial for safe aircraft operation. The interplay of weight, altitude, and air density significantly influences stall speed dynamics.
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Can someone explain how and why stall speed (TAS?) varies with aircraft weight and altitude? If you need equations to explain this, I can still handle algebra, but I have forgotten all of my college calculus! Thanks.
 
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If your weight increases, then the amount of lift you must produce increases. But your maximum obtainable CL does not change. So for the same CLmax the heavier aircraft would have to fly faster, so the stall speed would increase.

The stall speed varies with altitude because the density of the air varies with altitude. At a higher altitude the density decreases so again, for the same CLmax you must fly at a faster speed to achieve the same lift at a higher altitude.
 
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