The blades of the portable fan generate a 1.0-lb thrust T as shown. Compute the moment Mo of this force about the rear support point O. For comparison, determine the moment about O due to the weight of the motor-fan unit AB, whose weight of 7.7 lb acts at G. The moments are positive if counterclockwise, negative if clockwise. Assume a = 9.0 in., b = 1.5 in., c= 12.5 in., d=3.5in., e = 2.5 in., and 0 = 16⁰ Air flow

International Edition---engineering Mechanics: Statics, 4th Edition
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ISBN:9781305501607
Author:Andrew Pytel And Jaan Kiusalaas
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Chapter2: Basic Operations With Force Systems
Section: Chapter Questions
Problem 2.78P: A couple of magnitude 3601b ft is applied about portion AB of the drive shaft (the drive shaft is...
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The blades of the portable fan generate a 1.0-lb thrust T as shown. Compute the moment Mo of this force about the rear support point
O. For comparison, determine the moment about O due to the weight of the motor-fan unit AB, whose weight of 7.7 lb acts at G. The
moments are positive if counterclockwise, negative if clockwise.
Assume a = 9.0 in., b = 1.5 in., c= 12.5 in., d = 3.5in., e = 2.5 in., and 0 = 16%
Air flow
Answers:
Due to thrust T Mo=
Due to weight Mo=
B
15.574
i -22.626
lb-in.
Ib-in.
Transcribed Image Text:The blades of the portable fan generate a 1.0-lb thrust T as shown. Compute the moment Mo of this force about the rear support point O. For comparison, determine the moment about O due to the weight of the motor-fan unit AB, whose weight of 7.7 lb acts at G. The moments are positive if counterclockwise, negative if clockwise. Assume a = 9.0 in., b = 1.5 in., c= 12.5 in., d = 3.5in., e = 2.5 in., and 0 = 16% Air flow Answers: Due to thrust T Mo= Due to weight Mo= B 15.574 i -22.626 lb-in. Ib-in.
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