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 6 lb acts at G. The moments are positive if counterclockwise, negative if clockwise. Assume a = 8.5 in., b = 2.5 in., c = 11.5 in., d = 3.0in., e = 2.5 in., and 0 = 19° Air flow T d Answers: Due to thrust T Mo= i Due to weight Mo= i C Pak Pak B lb-in. lb-in.

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Chapter1: Units, Trigonometry. And Vectors
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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 6 lb acts at G. The
moments are positive if counterclockwise, negative if clockwise.
Assume a = 8.5 in., b = 2.5 in., c = 11.5 in., d = 3.0in., e = 2.5 in., and 0 = 19%
Air flow
d
106
b
Answers:
Due to thrust T Mo=
Due to weight Mo=
i
i
B
-T
lb-in.
lb-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 6 lb acts at G. The moments are positive if counterclockwise, negative if clockwise. Assume a = 8.5 in., b = 2.5 in., c = 11.5 in., d = 3.0in., e = 2.5 in., and 0 = 19% Air flow d 106 b Answers: Due to thrust T Mo= Due to weight Mo= i i B -T lb-in. lb-in.
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