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23 Nov 2019

<p>Calculate the ratio of the drag force on a jet flying at 874 km/h at an altitude of 11 km to the drag force on a prop-driven transport flying at half that speed and altitude. The density of air is 0.32 kg/m3 at 11 km and 0.64 kg/m3 at 5.5 km. Assume that the airplanes have the same effective cross-sectional area and drag coefficient C.</p>

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