Calculate the ratio of the drag force on a jet flying at 1020 km/h at an altitude of 9.5 km to the drag force on a prop-driven transport flying at half that speed and altitude. The density of air is 0.41 kg/m3 at 9.5 km and 0.68 kg/m³ at 4.8 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 1020 km/h at an altitude of 9.5 km to the drag force on a prop-driven transport flying at half that speed and altitude. The density of air is 0.41 kg/m3 at 9.5 km and 0.68 kg/m³ at 4.8 km. Assume that the airplanes have the same effective cross-sectional area and drag coefficient C.
University Physics Volume 1
18th Edition
ISBN:9781938168277
Author:William Moebs, Samuel J. Ling, Jeff Sanny
Publisher:William Moebs, Samuel J. Ling, Jeff Sanny
Chapter14: Fluid Mechanics
Section: Chapter Questions
Problem 95P: A skydiver will reach a terminal velocity when the air drag equals his or her weight. For a skydiver...
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