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Physics, 10.03.2020 06:41 triddi666

Calculate the ratio of the drag force on a jet flying at 957 km/h at an altitude of 7.9 km to the drag force on a prop-driven transport flying at half that speed and altitude. The density of air is 0.50 kg/m3 at 7.9 km and 0.73 kg/m3 at 4.0 km. Assume that the airplanes have the same effective cross-sectional area and drag coefficient C.

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Calculate the ratio of the drag force on a jet flying at 957 km/h at an altitude of 7.9 km to the dr...
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