The plane frame shown in Figure below is loaded by both concentrated and distributed loads. Moment MA is applied at pin support joint A, and load FB is applied at joint B. A uniform load with intensity q1 acts on member BC, and a linearly distributed load with peak intensity qo is applied downward on member ED. 1) Find the support reactions at joints A and D; then solve for internal forces at the top of member BC. 2) Plot the shear force and moment diagrams for all members. Use the numerical properties given below. a = 3 m, b = 2 m, c = 6 m, d=2.4 m, M₁ = 380 N m, FB =200 N, qo = 73 N/m, 91 = 146 N/m E 90 с X C D 91 d 3 4 B FB MA

Mechanics of Materials (MindTap Course List)
9th Edition
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Author:Barry J. Goodno, James M. Gere
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Chapter1: Tension, Compression, And Shear
Section: Chapter Questions
Problem 1.3.15P: 1.3-15 A space truss is restrained at joints A, B, and C, as shown in the figure. Load 2P is applied...
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pls add themoment and shear diagrams and the free body diagram, give a proper detailed solution

The plane frame shown in Figure below is loaded by both concentrated and
distributed loads. Moment MA is applied at pin support joint A, and load FB is
applied at joint B. A uniform load with intensity q1 acts on member BC, and a
linearly distributed load with peak intensity qo is applied downward on member
ED.
1) Find the support reactions at joints A and D; then solve for internal forces at
the top of member BC.
2) Plot the shear force and moment diagrams for all members.
Use the numerical properties given below.
a = 3 m, b = 2 m, c = 6 m, d=2.4 m, M₁ = 380 N m, FB =200 N, qo = 73 N/m,
91 = 146 N/m
E
90
с
X
C
D
91
d
3
4 B
FB
MA
Transcribed Image Text:The plane frame shown in Figure below is loaded by both concentrated and distributed loads. Moment MA is applied at pin support joint A, and load FB is applied at joint B. A uniform load with intensity q1 acts on member BC, and a linearly distributed load with peak intensity qo is applied downward on member ED. 1) Find the support reactions at joints A and D; then solve for internal forces at the top of member BC. 2) Plot the shear force and moment diagrams for all members. Use the numerical properties given below. a = 3 m, b = 2 m, c = 6 m, d=2.4 m, M₁ = 380 N m, FB =200 N, qo = 73 N/m, 91 = 146 N/m E 90 с X C D 91 d 3 4 B FB MA
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