A weight W 75 kN is applied eccentrically from the end of a cantilevered circular pipe of length L = 750 mm, as shown in the figure below. Points A and B lie in the vertical and horizontal axes, respectively, on a cross section located at a distance L₁= 350 mm from the end. The outer diameter is do 200 mm, the wall thickness is t= 5 mm, and a fluid in the pipe introduces a pressure p = 10 MPa. = 1. Calculate the absolute maximum normal and shear stresses at point A. 2. Calculate the absolute maximum normal and shear stresses at point B.

Mechanics of Materials (MindTap Course List)
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ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
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Chapter8: Applications Of Plane Stress (pressure Vessels, Beams, And Combined Loadings)
Section: Chapter Questions
Problem 8.3.11P: A standpipe in a water-supply system (see figure) is 12 ft in diameter and 6 in. thick. Two...
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Problem 4
A weight W = 75 kN is applied eccentrically from the end of a cantilevered circular pipe of
length L 750 mm, as shown in the figure below. Points A and B lie in the vertical and
horizontal axes, respectively, on a cross section located at a distance L₁ = 350 mm from the
end. The outer diameter is do = 200 mm, the wall thickness is t = 5 mm, and a fluid in the
pipe introduces a pressure p = 10 MPa.
1. Calculate the absolute maximum normal and shear stresses at point A.
2. Calculate the absolute maximum normal and shear stresses at point B.
L
Figure 4: Problem 4.
Transcribed Image Text:Problem 4 A weight W = 75 kN is applied eccentrically from the end of a cantilevered circular pipe of length L 750 mm, as shown in the figure below. Points A and B lie in the vertical and horizontal axes, respectively, on a cross section located at a distance L₁ = 350 mm from the end. The outer diameter is do = 200 mm, the wall thickness is t = 5 mm, and a fluid in the pipe introduces a pressure p = 10 MPa. 1. Calculate the absolute maximum normal and shear stresses at point A. 2. Calculate the absolute maximum normal and shear stresses at point B. L Figure 4: Problem 4.
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