Mechanics of Materials need help with this review I did and got parts of it wrong **Stress Analysis of Beam CB - Educational Content**___### Problem StatementBeam CB has some applied forces and moments such that the internal loadings at a cross-section through point A are:\[ V_y = -5 \text{kN} \]\[ M_x = +15 \text{kNm} \]The coordinate system used is \(P=0, V_{z} = 0, M_y = M_x =0\).### Given Data- **Shear Stress at Points D and E:** - \(| \tau_D | = 15 \text{MPa}\) - \(| \tau_E | = 12 \text {MPa}\)- **Normal Stress at Points D and E:** - \(| \sigma_D | = 24 \text {MPa}\) - \(| \sigma_E | = 30 \text {MPa}\)### TaskThe task is to translate this physical situation into correct stress elements at points D and E, i.e., for each point, fill in the magnitudes and directions of \(\sigma_x, \sigma_y,\) and \( \tau_{xy} \).### Steps to Follow:1. **Analyze Shear and Normal Stress:** - Determine the directions of shear and normal stresses at points D and E based on the given magnitudes. 2. **Diagram Interpretation:** - A schematic view of beam CB is depicted with a cross-sectional view taken at point A, indicating points D and E on the section. - Axes are defined with \(x\)-axis along the length of the beam, \(y\)-axis along the height, and \(z\)-axis into the plane.### Graphical Representation:- Two squares are provided below labeled D and E.- These squares represent elements at points D and E respectively, where you will fill in the stress components as per your analysis.#### Overview Diagram:- **Figure 1:** A simplified lateral view of beam CB, indicating point A with some loading applied.- **Figure 2:** An enlarged sectional view at point A highlighting points D and E, and the \(xyz\)-coordinate directions for stress analysis.### Drawing Section for Stress Elements:Use the provided squares to draw and annotate the stress elements, including the directions and magnitudes of \(\sigma_x, \sigma_y,\) and \( \tau_{xy}

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No explanation required Beam CB has some applied forces and moments such that the internal loadings at a cross-section through point A are: Vy = -5 kN and M₂ = + 15 kNm (P=0, V₂ = 0, My = Mx=0), for the coordinate system shown. ay. You have already done the analysis (using the shear and flexure formulae) and found that the magnitude of the shear stress at points D and E are B |TD| = 15 MPa and |TE| = 12 MPa -D and the magnitudes of the normal stress at points D and E are |op| = 24 MPa and |OE| = 30 MPa. Your job is to translate this physical situation into correct stress elements at points D and E, i.e. for each point you will fill in magnitudes and directions of ox, Gy, and Txy. Draw the stress elements at D and E. D: E: 201 + Some loading B

No explanation required Beam CB has some applied forces and moments such that the internal loadings at a cross-section through point A are: Vy = -5 kN and M₂ = + 15 kNm (P=0, V₂ = 0, My = Mx=0), for the coordinate system shown. ay. You have already done the analysis (using the shear and flexure formulae) and found that the magnitude of the shear stress at points D and E are B |TD| = 15 MPa and |TE| = 12 MPa -D and the magnitudes of the normal stress at points D and E are |op| = 24 MPa and |OE| = 30 MPa. Your job is to translate this physical situation into correct stress elements at points D and E, i.e. for each point you will fill in magnitudes and directions of ox, Gy, and Txy. Draw the stress elements at D and E. D: E: 201 + Some loading B

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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