An airplane has a mass of 25 Mg and its engines develop a total thrust of 40
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An airplane has a mass of 25 Mg and its engines develop a total thrust of 40 kN during take-off. If the drag D exerted on the plane has a magnitude D = 2.25v2, where v is expressed in meters per second and D in new-tons, and if the plane becomes airborne at a speed of 240 km/h, determine the length of runway required for the plane to take off?
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Related Book For
Vector Mechanics for Engineers Statics and Dynamics
ISBN: 978-0073398242
11th edition
Authors: Ferdinand Beer, E. Russell Johnston Jr., David Mazurek, Phillip Cornwell, Brian Self
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