give handwritten solution to this please The rigid bar BDE is welded at point B to the steel beam AC. For the loading shown below.1. Derive the bending moment equation for the beam using Macaulay's notation.2. Determine the slope at point A3. Determine the deflection at point BAssume EI of the beam is constant.B20 kN/mE60 kN1.5 m-1.5 m-1.5 m-C

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Answered: The rigid bar BDE is welded at point B…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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For the steel cantilevered beam shown, determine the minimum moment of inertia of the structural tee section, Imin if the deflection at the free end is limited to 1.2 in. -L2 Given: .L=19.6 ft • L₂ = 6.6 ft F = 1200 lb • q = 1.05 kip/ft Imin=-512.6 79 - ¹/2 |F L +4₂+ L2 H q a
Given the Cantilever beam loaded as shown, determine the deflection of the beam at the right end by using Three Moment Equation (TME). Note: The unit obtained from TME for EIy is kips-ft^3.
For the beam and loading shown, use discontinuity functions to compute: (a) the deflection VA of the beam at A, and (b) the deflection Vmidspan of the beam at midspan (i.e., x = 2.45 m). Assume a constant value of El = 1270 kN-m² for the beam; M₁ = 9 kN-m, wo = 19.8 kN/m, LAB = 1.1 m, LBc = 2.7 m. MA A Answer: (a) VA = (b) Vmid i LAB i Wo B LBC mm. mm.
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determine the deflection at B in mm using Conjugate Beam Method. Consider 150 mm x 200 (b x h) mm section and E=80 GPa. Enter the absolute value only and round off your answer to 3 decimal places Answer asap. I rate
Problem 2 Moment-Area Method: For the given beam below, answer the questions. El = constant: 5 kN 8 kN-m A В 6 m 6 m 6 m (b) (c) | Draw the Curvature Diagram of the beam. Mark all important values. Determine the slope at point A, 64, using the moment-area method. | Determine the deflection at point B, Ag, using the moment-area method.
Determine the deflection at point C of the beam shown in by the moment-area method.
If w = 25 kN/m., calculate the value of EIδ at 1 m. of the free end of the loaded beam as indicated in the figure below
The cantilever beam shown is subjected to a concentrated load of P=70800 lb. The cross-sectional dimensions and the moment of inertia of the W16x57 wide-flange shape are: d = 16.4 in. tw=0.430 in. by=7.12 in. ty=0.715 in. 1₂-758 in.4 Compute the value of the shear stress at point H, located at y = 4.8 in. below the centroidal xis. H Answer: Shear stress = psi
Determine the value of the applied torque, M if the beam's midspan deflection is to be zero. Assume El=const. Sketch SHEAR / MOMENT / DISPLACEMENT diagrams. P = 100 lb 2 ft M w=10 lb/ft 3 ft 5 ft B
Using any Geometric Methods only: (Double Integration, Conjugate Beam, Area Moment) Determine the deflection (mm) of the beam at point B. Round off your final answer in 2 decimal places P kN w kN /m A C X2 EI Given: P = 25 kN W = 12 kN/m X1 = X2 = E = 200000 MPa x 106 = 600 mm4 5.

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