An element in plane stress from the fuselage of an airplane is subjected to compressive stresses of magnitude 22 MPa in the horizontal direction and tensile stresses of magnitude 6.0 MPa in the vertical direction. Also, shear stresses of magnitude 11.0 MPa act in the directions shown (see the figure)

Mechanics of Materials (MindTap Course List)
9th Edition
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Barry J. Goodno, James M. Gere
Chapter7: Analysis Of Stress And Strain
Section: Chapter Questions
Problem 7.3.8P: An element in plane stress from the fuselage of an airplane is subjected to compressive stresses of...
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An element in plane stress from the fuselage of an airplane is subjected to compressive stresses of magnitude 22 MPa in the horizontal direction and tensile stresses of magnitude 6.0 MPa in the vertical direction. Also, shear stresses of magnitude 11.0 MPa act in the directions shown (see the figure).

An element in plane stress from the fuselage of an airplane is subjected to compressive stresses of magnitude 22 MPa in the horizontal direction and tensile stresses of magnitude 6.0 MPa in the vertical direction.
Also, shear stresses of magnitude 11.0 MPa act in the directions shown (see the figure).
6.0 MPa
22 MPa
11.0 MPa
(a)
(b)
Determine the maximum shear stresses and associated normal stresses. (Enter your answers in MPa. For the shear stress, enter the magnitude. For the normal stresses, use the deformation sign convention.
Consider only the stresses in the plane of the element.)
Tmax
MPа
Ox1
MPa
MPa
Show them on a sketch of a properly oriented element. (Submit a file with a maximum size of 1 MB.)
Transcribed Image Text:An element in plane stress from the fuselage of an airplane is subjected to compressive stresses of magnitude 22 MPa in the horizontal direction and tensile stresses of magnitude 6.0 MPa in the vertical direction. Also, shear stresses of magnitude 11.0 MPa act in the directions shown (see the figure). 6.0 MPa 22 MPa 11.0 MPa (a) (b) Determine the maximum shear stresses and associated normal stresses. (Enter your answers in MPa. For the shear stress, enter the magnitude. For the normal stresses, use the deformation sign convention. Consider only the stresses in the plane of the element.) Tmax MPа Ox1 MPa MPa Show them on a sketch of a properly oriented element. (Submit a file with a maximum size of 1 MB.)
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