Current Attempt in Progress The blades of the portable fan generate a 1.7-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 15.7 lb acts at G. The moments are positive if counterclockwise, negative if clockwise. Assume a = 7.5 in., b = 2.5 in., c = 13.0 in., d = 3.5in., e = 1.5 in., and 0 = 15⁰ Air flow T e d O b Answers: Due to thrust T Mo= Due to weight Mo= i lb-in. lb-in.

Current Attempt in Progress The blades of the portable fan generate a 1.7-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 15.7 lb acts at G. The moments are positive if counterclockwise, negative if clockwise. Assume a = 7.5 in., b = 2.5 in., c = 13.0 in., d = 3.5in., e = 1.5 in., and 0 = 15⁰ Air flow T e d O b Answers: Due to thrust T Mo= Due to weight Mo= i lb-in. lb-in.

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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