Engineering Fundamentals
Engineering Fundamentals
6th Edition
ISBN: 9780357112144
Author: Saeed Moaveni
Publisher: MISC PUBS
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Chapter 17, Problem 32P
To determine

The ratio of power required when the plane is cruising at 8000m and when the plane is cruising at 11000m.

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An aircraft is flying in level flight at a speed of 200 km/h through air (density, p = 1.2 kg/m³, and viscosity, µ = 1.6 x 10-5 N-s/m²). The lift coefficient at this speed is 0.4 and the drag coefficient is 0.0065. The mass of the aircraft is 800 kg. The effective lift area of the aircraft is
Q- An automobile with projected area 2.6 m² is running on a road with a speed of 120 km per hour. The mass density and the kinematic viscosity of air are 1.2 kg/m² and 1.5 × 10-5 m²/s, respectively. The drag coefficient is 0.30. Find the drag force on the automobile.
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