Consider the beam given in the figure. Given: X= 18 kN and Eis constant.NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part.w = 4 kN/m216 mBhinge3 m.C16 m-3m-ADDraw the shear and moment curves for the beam given in the figure.

Answered: Image /qna-images/answer/daad31b0-cae7-49dc-ba49-90128c8f2a23.jpg

Answered: Consider the beam given in the figure.…

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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T (Shear force) and M (Bending) for the system whose loading condition is given in Figure 1.Draw the moment diagrams. Calculate the deflection (vertical displacement) at point B in mm using Castigliano's Theorem. The beam bending stiffness (EI) is constant along the bar and its value is 50 000 kNm2.q=1,4(kN/m)a=8(m)El=50000(kNm2)
Upvote will be given. Please write the solutions legibly. Solve in 2 decimal places. 15 KN 20 KN/m 4m B 1m FIGURE 2 200 mm 50 100 mm 50 m 75mm 200 mm A. What is the maximum internal shear force of the beam in FIGURE 2? B. What is the maximum internal bending moment of the beam in FIGURE 2?
Solve the following problem found in the image below. Draw the forces in the following order: 100#, 145#, 200# (all tip-to-tail). Solve for the Resultant using the two different methods listed below. Create a different sketch for each of the methods. The answer for the resultant for both of the following methods must include the magnitude and the direction of the resultant (relative to horizontal - positive x, in a counter-clockwise direction). 1. Method 1: Solve Graphically using an engineer's scale and protractor. Use Scale 1"=100 pounds. 2. Method 2: Solve Mathematically (using the Cosine Law & the Sine Law).
A beam is loaded and supported as shown. (a) Use the double-integration method to determine the reactions at supports A and C. Reaction forces are positive upwards and couples are positive counter-clockwise unless otherwise stated. (b) Draw the shear-force and bending-moment diagrams for the beam. Assume w = 25 kN/m, L = 12.6 m and El = 5.7 x 104 kN-m² is constant for the beam. A Answer: (a) Ay = i Cy= i Mc = i (b) Vmax Mmax = i i W L/2 B L/2- ! kN ! kN kN•m KN kN.m
Required Information Consider the beam given in the figure. Given: X= 18 kN and Eis constant. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. A w = 4 kN/m 21 hinge - 6 m3 m I 6 m 3 m- Draw the shear and moment curves for the beam given in the figure.
Use discontinuity functions to develop the load function w(x) for the beam shown. Include the beam reactions in this expression. Integrate w(x) twice to determine V(x) and M(x), and use these functions to plot the shear-force and bending-moment diagrams on paper. Use these plots to answer the questions in the subsequent parts of this GO exercise. Let a = 2.75 m, b = 4.00 m, c=1.75 m, Wg = 20 kN/m and wc = 55 kN/m. WC WR b Calculate the reaction forces A, and Dy acting on the beam. Positive values for the reactions are indicated by the directions of the red arrows shown on the free-body diagram below. (Note: Since A, = 0, it has been omitted from the free-body diagram.) WC y A B C A D |Dy Incorrect Use your shear-force equation V(x) to find the location where V= 0 between points B and C. Alternatively, note that the shear force at B in this case is known from Part 3. Recall that the change in the shear force between any two locations is equal to the area under the distributed-load curve…
An indeterminate beam carries a trapezoidal load as shown in the figure. Using Moment Distribution Method (up to 4th distribution), solve the following: Let w = 160KN/m (NOTE: Put a negative sign if the moment is CCW otherwise don't put any sign at all. Don't also put any units. Express ALL YOUR FINAL ANSWERS to at least 5decimal places) 11w 4m Sm Solve the Moment at span BC. Solve the Moment at span CB. Solve the Moment at span CD. Solve the Moment at span DC. Solve the Moment at span AB. III () ()
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Consider a 150-mm-long segment of a simply supported beam. The internal bending moments on the left and right sides of the segment are 70 kN-m and 76 kN-m, respectively. The cross-sectional dimensions of the flanged shape are shown in the accompanying figure. Assume b1 = 155 mm, b2 = 30 mm, b3 = 265 mm, d1 = 65 mm, d2 = 220 mm, d3 = 65 mm. Determine the maximum horizontal shear stress in this segment of the beam.
Consider a 110-mm-long segment of a simply supported beam. The internal bending moments on the left and right sides of the segment are 55 kN-m and 61 kN-m, respectively. The cross-sectional dimensions of the flanged shape are shown in the accompanying figure. Assume b1 = 165 mm, b2 = 45 mm, b3 = 265 mm, d1 = 65 mm, d2 = 240 mm, d3 = 65 mm. Determine the maximum horizontal shear stress in this segment of the beam.

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Consider the beam given in the figure. Given: X= 18 kN and Eis constant. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. w = 4 kN/m 21 6 m B hinge 3 m. C 1 6 m -3m- AD Draw the shear and moment curves for the beam given in the figure.