An element in plane stress from the fuselage of an airplane is subjected to compressive stresses of magnitude 20 MPa in the horizontal direction and tensile stresses of magnitude 5.0 MPa in the vertical direction. Also, shear stresses of magnitude 11.0 MPa act in the directions shown (see the figure). 5.0 MPa 20 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 the plane of the element.) Tmax = MPa MPa y1 = MPa Show them on a sketch of a properly oriented element. (Submit a file with a maximum size of 1 MB.) Choose File No file chosen

An element in plane stress from the fuselage of an airplane is subjected to compressive stresses of magnitude 20 MPa in the horizontal direction and tensile stresses of magnitude 5.0 MPa in the vertical direction. Also, shear stresses of magnitude 11.0 MPa act in the directions shown (see the figure). 5.0 MPa 20 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 the plane of the element.) Tmax = MPa MPa y1 = MPa Show them on a sketch of a properly oriented element. (Submit a file with a maximum size of 1 MB.) Choose File No file chosen

Materials Science And Engineering Properties

1st Edition

ISBN:9781111988609

Author:Charles Gilmore

Publisher:Charles Gilmore

Chapter9: Time, Temperature, And Mechanical Properties

Section: Chapter Questions

Problem 9.3P

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