The conversation between human and AI assistant.
How do you calculate the stall speed of an aircraft?
Yes, please! Can you tell me what the formula is?
Of course! The formula is: Vstall = √[(2*w)/(ρ*Clmax*S)], where Vstall is the stall speed, w is the weight of the aircraft, ρ is the density of the air, S is the wing area, and Clmax is the maximum lift coefficient.