Calculate the ratio of the drag force on a jet flying at 878 km/h at an altitude of 9.8 km to the drag force on a prop-driven transport flying at half that speed and altitude. The density of air is 0.39 kg/m3 at 9.8 km and 0.68 kg/m3 at 4.9 km. Assume that the airplanes have the same effective cross-sectional area and drag coefficient C.
Calculate the ratio of the drag force on a jet flying at 878 km/h at an altitude of 9.8 km to the drag force on a prop-driven transport flying at half that speed and altitude. The density of air is 0.39 kg/m3 at 9.8 km and 0.68 kg/m3 at 4.9 km. Assume that the airplanes have the same effective cross-sectional area and drag coefficient C.
Principles of Physics: A Calculus-Based Text
5th Edition
ISBN:9781133104261
Author:Raymond A. Serway, John W. Jewett
Publisher:Raymond A. Serway, John W. Jewett
Chapter5: More Applications Of Newton’s Laws
Section: Chapter Questions
Problem 40P
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Calculate the ratio of the drag force on a jet flying at 878 km/h at an altitude of 9.8 km to the drag force on a prop-driven transport flying at half that speed and altitude. The density of air is 0.39 kg/m3 at 9.8 km and 0.68 kg/m3 at 4.9 km. Assume that the airplanes have the same effective cross-sectional area and drag coefficient C.
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