Structural Analysis
6th Edition
ISBN: 9781337630931
Author: KASSIMALI, Aslam.
Publisher: Cengage,
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The canitlevered beam is fixed on the left end and is subjected to the triangular distributed load as shown. Using the double integration method, determine: (a) the formula for slope and deflection with respect to x, (b) The slope and deflection at point B, at the right end of the beam. X=0 at the fixed connection, and x is positive to the right.
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- (1) Determine the equations of the elastic curve for the beam using the x and x2 coordinates. Then, find the deflection under the load P. EI is constant. Larrow_forwardSubject is structural analysis Please show each steps to the question and make it easy for me to understand. Explain the diagramarrow_forwardSolve the problem by the moment-area method. The beam has constant flexural rigidity EI. A simple beam AB supports two concentrated loads P at the positions shown in the figure. B C 4. 4 A support C at the midpoint of the beam is positioned at distance d below the beam before the loads are applied. Assuming that d = 12 mm, L = 5.4 m, E = 200 GPa, and I = 193 x 10° mm, calculate the magnitude of the loads P (in kN) so that the beam just touches the support at C. 163.87 x kNarrow_forward
- Considering the solution above, can you help with part (d) 3. The beam shown below has a Young’s modulus of 50 GPa and has a square cross-section of side1 cm. Determine the following using the second-order integration method:(a) Bending moment M(x) along the length of the beam.(b) The slope of the beam θ(x).(c) The deflection of the beam v(x).(d) Slope of the beam at support θBarrow_forwardFor the beam shown, obtain: A). Applying the double integration method, the rotation in the left support (A), and the deflection in (C). B). Applying the moment of area method, the rotation in (D), and the maximum deflection between supports A and B. C). Applying the conjugate beam method, the rotation in (B), and the deflection in (D). Use the following Values: a = 1.75 m, q = 2.25 kN/m. E = 200 Gpa, |= 200 x10^6 mm^4 Note: Please provide the deflection results in mm and rotation in degrees. 90² qa A B D C аarrow_forward
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