2. A steel plate (dimension in mm) is loaded and supported as shown in Figure 2. Assume that a downward settlement of 0.01 mm occurs at support 2. Using the finite element method with two 3-noded triangular elements, determine the horizontal and vertical displacements of the plate at the right top corner. Young's modulus E = 200GPA Poisson's ratio v = 0.3 Plate thickness t= 5mm 5kN %3D

Structural Analysis
6th Edition
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Author:KASSIMALI, Aslam.
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Chapter2: Loads On Structures
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2. A steel plate (dimension in mm) is loaded and supported as shown in Figure 2. Assume
that a downward settlement of 0.01 mm occurs at support 2. Using the finite element
method with two 3-noded triangular elements, determine the horizontal and vertical
displacements of the plate at the right top corner.
Young's modulus E = 200GPA
Poisson's ratio v = 0.3
5kN
Plate thickness t= 5mm
0.03m
0.01 m
0.05 m
Figure 2
Note: if the connectivity of element 1 is 1-2-3 and element 2 is 1-3-4, the stiffness
matrices of elements 1 and 2 can be calculated as (using the units m and N):
0.110
0.000 -0.110
0.165
0.000 -0.165
0.000
0.038 0.192
-0.038 -0.192
0.000
[K]] = 10°x
-0.110
0.192
1.071
-0.357
-0.962
0.165
0.165 -0.038 -0.357
2.786
0.192 -2.747
0.000
-0.192
-0.962
0.192
0.962
0.000
-0.165
0.000
0.165
-2.747
0.000
2.747
0.467
0.238
-0.220
-0.192
-0.247
-0.046
0.238
0.967
-0.165
-0.077
-0.073 -0.890
[K2] = 10° x
-0.220 -0.165
0.330
0.000
-0.110
0.165
-0.192 -0.077
0.000
0.115
0.192 -0.038
-0.247
-0.073
-0.110
0.192
0.357
-0.119
-0.046
-0.890
0.165
-0.038
-0.119
0.929)
Transcribed Image Text:2. A steel plate (dimension in mm) is loaded and supported as shown in Figure 2. Assume that a downward settlement of 0.01 mm occurs at support 2. Using the finite element method with two 3-noded triangular elements, determine the horizontal and vertical displacements of the plate at the right top corner. Young's modulus E = 200GPA Poisson's ratio v = 0.3 5kN Plate thickness t= 5mm 0.03m 0.01 m 0.05 m Figure 2 Note: if the connectivity of element 1 is 1-2-3 and element 2 is 1-3-4, the stiffness matrices of elements 1 and 2 can be calculated as (using the units m and N): 0.110 0.000 -0.110 0.165 0.000 -0.165 0.000 0.038 0.192 -0.038 -0.192 0.000 [K]] = 10°x -0.110 0.192 1.071 -0.357 -0.962 0.165 0.165 -0.038 -0.357 2.786 0.192 -2.747 0.000 -0.192 -0.962 0.192 0.962 0.000 -0.165 0.000 0.165 -2.747 0.000 2.747 0.467 0.238 -0.220 -0.192 -0.247 -0.046 0.238 0.967 -0.165 -0.077 -0.073 -0.890 [K2] = 10° x -0.220 -0.165 0.330 0.000 -0.110 0.165 -0.192 -0.077 0.000 0.115 0.192 -0.038 -0.247 -0.073 -0.110 0.192 0.357 -0.119 -0.046 -0.890 0.165 -0.038 -0.119 0.929)
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