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An airplane propeller is 2.08 m in length (from tip to

University Physics | 13th Edition | ISBN: 9780321675460 | Authors: Hugh D. Young, Roger A. Freedman ISBN: 9780321675460 31

Solution for problem 34E Chapter 10

University Physics | 13th Edition

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University Physics | 13th Edition | ISBN: 9780321675460 | Authors: Hugh D. Young, Roger A. Freedman

University Physics | 13th Edition

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Problem 34E

An airplane propeller is 2.08 m in length (from tip to tip) and has a mass of 117 kg. When the airplane’s engine is first started, it applies a constant torque of 1952 N · m to the propeller, which starts from rest. (a) What is the angular acceleration of the propeller? Model the propeller as a slender rod and see Table 9.2. (b) What is the propeller’s angular speed after making 5.00 revolutions? (c) How much work is done by the engine during the first 5.00 revolutions? (d) What is the average power output of the engine during the first 5.00 revolutions? (e) What is the instantaneous power output of the motor at the instant that the propeller has turned through 5.00 revolutions?

Step-by-Step Solution:

Solution 34E Step 1: Given data: Constant torque = 1952 N/m Length of airplane propeller from tip to tip l = 2.08 m Mass of propeller M = 117 kg Step 2: Torque is given by = I 2 Moment of inertia of propeller is given by I = 1/12 ML 2 I = 1/12 (117 kg)(2.08 m) 2 I = 42.18 kg/m Step 3: (a).Angular acceleration of the propeller is given by = /I 2 = (1952 N/m)/(42.18 kg/m ) 2 = 46.27 rad/s Step 4: (b).The propeller angular speed after making 5.00 revolution is given by 2 w = w +02 Where = 2 5.0* radand w = 0 0 w = 2 w = 2(46.27 rad/s )(2 5*00 rad) w = 53.91 rad/sec

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Chapter 10, Problem 34E is Solved
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Textbook: University Physics
Edition: 13
Author: Hugh D. Young, Roger A. Freedman
ISBN: 9780321675460

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