Use the graphical method to construct the shear-force and bending-moment diagrams for the beam shown. Let a = 2.7 ft, b = 8.1 ft, c = 3.6 ft, MA = 6600 lb-ft, P = 2000 lb, and w=520 lb/ft. Label all significant points on each diagram and identify the maximum moments (both positive and negative) along with their respective locations. Clearly differentiate straight-line and curved portions of the diagrams. Determine the maximum shear force and bending moment in the beam.

Use the graphical method to construct the shear-force and bending-moment diagrams for the beam shown. Let a = 2.7 ft, b = 8.1 ft, c = 3.6 ft, MA = 6600 lb-ft, P = 2000 lb, and w=520 lb/ft. Label all significant points on each diagram and identify the maximum moments (both positive and negative) along with their respective locations. Clearly differentiate straight-line and curved portions of the diagrams. Determine the maximum shear force and bending moment in the beam.

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Similar questions

1.1 A beam ABC 12 m long is simply supported at A and B where AB = 8 m. Point loads of 15 kN and 6 kN are applied at the mid-point of AB and at C respectively. A uniformly distributed load of 4 kN/m extends for 6 m from A. Determine the values of the reactions by resolving and taking moments. Check your results by using virtual work, Sketch the shear-force and bending-moment diagrams and find the values under the point loads.
The beam with cross-section shown in Figure 1 is subjected to a uniformly distributed load and a moment. The centroidal axis of the section is c= 74.44 mm from the bottom. I. -2.18x10 mm. E = 2.1×10 MPa. a) At a cross-section 2 m to the right of support A; i) ii) iii) Calculate the Shear Force, V, and the Bending Moment, M. Determine the maximum bending stress. Sketch the bending stress distribution across the section, include critical tension & compression stress values. Determine shear stress developed at the flange-web interface and also the shear stress at the neutral axis of the cross-section. Sketch the shear stress distribution across the section, include the critical values. b) Using the double integration method, find the deflection curve for 0≤x≤5 m. 3 kN/m 5m 3 m- Figure 1 15 kN-m 100 All dimensions are in mm.
Theory of structure L=10 ft Udl =4k/ft
Question 3 Determine the deflections in horizontal and vertical directions at point C and the reactions at supports A and B of the truss shown in Figure (3) using the stiffness method. Take E = 210 GPa and A = 170 mm² for all members. 24 KN 3.00 m 4.00 m Figure (3) C B 18 KN
Calculate the forces in all members using equilibrium of joint, ALso check weather the member is in tension or in compression. only HANDWRITTEN answer needed ( NOT TYPED)
Please give me correct answer someone give wrong answers
I need the answer as soon as possible
Solve the problem and answer the questions that follow. - If the supports were swapped such that the left support were a roller and the right support a pin, how would your solution change? - If the value of “w” were doubled, what would be the bending moment at the left most point of the beam?
Solve the magnitude and position of the missing force, make sure to do it in step by step manner and make sure to illustrate properly For the given beam shown. There are three forces acting on the beam and the third force is missing, if the resultant of these three vertical forces is 13.6 N acting up at 3 meters to the right of A. Determine the magnitude and position of the missing force.
Q6.1. For the two-dimensional truss structure shown in the figure, determine all the nodal deflections and nodal forces. The support reaction forces, Rix, Rly and R3x are also indicated on this figure next to the supports. Both bar members (1) and (2) are of length 2.0 m. Each member has a cross-sectional area of 80 mm² and a modulus of elasticity of 200 GPa, Ignore the possibility of buckling in the compression members. Ans.: u2x=0.625 mm, u2y=-2.061, u3y=-0.375 mm, Rix--5 kN, R₁-3 kN, R3x=3 kN. R R RIS (1) (3) Fig. 1 3 kN 2 kN X
Calculate for the shear force in kN at member ED of the frame shown in figure 1 using Portal Method. Enter absolute value and use 2 decimal places in your solution.
Q.2) (a) Calculate the support reactions of the loaded beam shown below. (b) Write equations for w(x), V(x) and M(x) of the beam using singularity functions. (c) Sketch the shear-force and bending moment diagrams for the beam for the beam using the Graphical method. Label the values of shear-force and bending-moment at all key points. 350 N.m G 0.5 m4 2m 95 N/m, 200 N 250 N.m 80 N/m 2m 300 N 0.5 m