Engineering, 12.02.2020 05:30 kassimh495

An airplane of weight W and wing area S flies level at speed V while executing a turn of constant radius R. The wing can pull a maximum lift coefficient CLmax before stall. Derive the formula for the turn radius versus flight speed at this maximum lift coefficient. This radius represents the tightest turn the airplane can make at the given flight speed. Plot 1/R versus V for the airplane in Problem 2A. When 1/R = 0 do you get the correct limit of level flight stall speed? Hint: In a steady turn the lift must equal the resultant of the weight vector and the centrifugal force vector.

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An airplane of weight W and wing area S flies level at speed V while executing a turn of constant ra...

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