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.