QUESTION 1 (a) Sketch a bar element, a plane truss element, and a beam element. Label the axes, nodes and nodal degrees of freedom (dof). Identify the physical quantity of each dof. (b) Figure Q1(a) below shows a loaded cantilevered beam. The beam is made of a material with E = 200 GPa while the cross section of the beam is shown in Figure Q1(b).
QUESTION 1 (a) Sketch a bar element, a plane truss element, and a beam element. Label the axes, nodes and nodal degrees of freedom (dof). Identify the physical quantity of each dof. (b) Figure Q1(a) below shows a loaded cantilevered beam. The beam is made of a material with E = 200 GPa while the cross section of the beam is shown in Figure Q1(b).
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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![QUESTION 1
(a) Sketch a bar element, a plane truss element, and a beam element. Label the axes, nodes and
nodal degrees of freedom (dof). Identify the physical quantity of each dof.
(b) Figure Q1(a) below shows a loaded cantilevered beam. The beam is made of a material
with E = 200 GPa while the cross section of the beam is shown in Figure Q1(b).
کسیس
2 kN/m
1
6 m
10 KN
(a)
2
4 m
8 kN
40 kN-m
Figure Q1
200 mm
(b)
400 mm](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fb8a9802b-ded9-4a7b-93c8-71218002814a%2Ff5e06e96-7c8b-47ba-bd2f-e1bfc3e2738d%2Fpz1gehi_processed.jpeg&w=3840&q=75)
Transcribed Image Text:QUESTION 1
(a) Sketch a bar element, a plane truss element, and a beam element. Label the axes, nodes and
nodal degrees of freedom (dof). Identify the physical quantity of each dof.
(b) Figure Q1(a) below shows a loaded cantilevered beam. The beam is made of a material
with E = 200 GPa while the cross section of the beam is shown in Figure Q1(b).
کسیس
2 kN/m
1
6 m
10 KN
(a)
2
4 m
8 kN
40 kN-m
Figure Q1
200 mm
(b)
400 mm
![By using two (2) beam elements to model the beam, the nodal degrees of freedom are:
NODE 2
NODE 3
-0.014
-0.031
-0.004
-0.005
Deflection (m)
Rotation (radian)
NODE 1
0
0
At a section 3 m from the fixed end of the beam, calculate by using finite element method:
(i) the deflection;
(ii) the shear force;
(iii) the bending moment;
(iv) the maximum bending stress.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fb8a9802b-ded9-4a7b-93c8-71218002814a%2Ff5e06e96-7c8b-47ba-bd2f-e1bfc3e2738d%2Fauu677_processed.jpeg&w=3840&q=75)
Transcribed Image Text:By using two (2) beam elements to model the beam, the nodal degrees of freedom are:
NODE 2
NODE 3
-0.014
-0.031
-0.004
-0.005
Deflection (m)
Rotation (radian)
NODE 1
0
0
At a section 3 m from the fixed end of the beam, calculate by using finite element method:
(i) the deflection;
(ii) the shear force;
(iii) the bending moment;
(iv) the maximum bending stress.
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Step 1: Introduce the problem statement
VIEWStep 2: State the characteristics of bar, truss and beam element
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VIEWStep 3: Determine flexural rigidity of the beam
VIEWStep 4: Formulate element stiffness matrices
VIEWStep 5: Formulate global stiffness matrix
VIEWStep 6: Formulate load vector matrix
VIEWStep 7: Formulate displacement vector
VIEWStep 8: Determine joint displacement
VIEWStep 9: Determine support reactions
VIEWStep 10: Compute maximum bending stress
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