Determine stress components acting on the inclined plane AB shown in Figure 1. The directions of the stress components are as indicated in Figure 1. 50 MPa A 30 MPа 70 MPа 50° B
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Q: Using Mohr's circle, determine stress components on an element oriented 60 ° counter- clockwise with…
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Q: Determine stress components acting on the inclined plane AB shown in Figure 1. The directions of the…
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- -26 A rectangular plate of dimensions 125 mm × 75 mm is subjected to tensile stress sy= 67 kPa and compressive stress a. If it is known that the normal stress along the diagonal t—t is ??t= -6.57 kPa, find stress ??y on element A. aAn clement m plane stress from the frame of a racing car is oriented at a known angle 8 (sec figure). On this inclined clement, the normal and shear stresses have the magnitudes and directions shown in the figure. Determine the normal and shear stresses acting on an clement whose sides are parallel to the \y axes, that is, determine crv, tr(_, and t, Show the results on a sketch of an clement oriented at B .An clement m plane stress from the frame of a racing car is oriented at a known angle 8 (sec figure). On this inclined clement, the normal and shear stresses have the magnitudes and directions shown in the figure. Determine the normal and shear stresses acting on an clement whose sides are parallel to the xy axes, that is, determine crv, tr(_, and t. Show the results on a sketch of an clement oriented at B = 10
- The polyethylene liner of a settling pond is subjected to stresses ax= 350 psi. a = 112 psi. and = -120 psi, as shown by the plalte-stress element in the figure part a. Determine the normal and shear stresses acting on a seam oriented at an angle 01300 to the element, as shown in the figure part b. Show these stresses on a sketch of an element having its sides parallel and perpendicular to the seam.At a point on the surface of an elliptical exercise machine, the material is in biaxial stress with t = 1400 psi and trv = —900 psi, as shown in the figure part a. The figure part b shows an inclined plane aa cut through the same point in the material but oriented at an angle ft Determine the value of the angle 6 between zero and 90° such that no normal stress acts on plane aa. Sketch a stress clement having plane aa as one of its sides and show all stresses acting on the clementAn element in plane stress on the fuselage of an airplane (figure part a) is subjected to compressive stresses with a magnitude of 42 MPa in the horizontal direction and tensile stresses with a magnitude of 9.5 MPa in the vertical direction (sec figure part b). Also, shear stresses with a magnitude of 15.5 MPa act in the directions shown. Determine the stresses acting on an element oriented at a clockwise angle of 40g from the horizontal. Show these stresses on a sketch of an element oriented at this angle.
- The stresses acting on an element are x= 750 psi, y= 600 psi, and xy = 400 psi. Determine the principal stresses and show them on a sketch of a properly oriented element.Determine the equivalent state of stress on an element at the same point oriented 60 degrees clockwise with respect to the element shown in the figure below. Suppose that Sigma-x = 151 MPa, Sigma-y= 106 MPa. Determine sigma-x' in MPa. Express your answer to three significant figures. Do not include the units with your answers.The state of stress at a point in a member is shown on the rectangular stress element in (Figure 5) where the magnitudes of the stresses are |σx|=11 ksi, |σy|=31 ksi, and |τxy|=17 ksi. Determine the state of stress on an element rotated 50∘ counterclockwise from the element shown. Answers should be as σx′=, σy′=, τx′y′= in ksi
- The state plane stress at a point is represented by the stress element below. Determine the stresses acting on an element oriented 30 degree counterclockwise respect to the original element. 1. Calculate the normal stress at the x-axis a. 69.8 MPa b. 75.25 MPa c. -39.8 MPa d. -24.60 MPa 2. Calculate the normal stress at the y-axis a. -39.8MPa b. 69.8 MPa c. -24.60 MPa d. 75.60 MPa 3. Calculate the shearing stress at the xy-face a. 55 MPa b. -55 MPa c. 65 MPa d. -65 MPaThe state of stress at a point in a member is shown on the rectangular stress element in (Figure 4) where the magnitudes of the stresses are |σx|=137 MPa and |τxy|=70 MPa. Determine the state of stress on an element rotated 85∘ clockwise from the element shown. Answer should be listed as σx′=, σy′=, τx′y′= in MPaMohr's Circle The major and minor principal stresses acting at a point are 80 psi compression and 20 psi tension. (a) Draw the Mohr's circle for this stress combination. (b) What is the maximum shear stress acting at the point, and what value of normal stress acts on the plane? (c) Determine the value of the shear and normal stress acting on a plane that is 30° from the major principal plane. kindly answer the following with a complete solution so that i can understand how to solve it. thank you