A processing method of a steel structure fiber model
A fiber model and processing method technology, applied in data processing applications, electrical digital data processing, special data processing applications, etc., can solve the problems of inconsistency in the damage degree index, insufficient to reflect the damage form of components, etc., to achieve simple analysis process, The effect of high work efficiency
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Embodiment 1
[0044] The section steel is H680×400×32×32, and its material strength is the main beam ZL of Q345 1 As an example, γ=1.16 is calculated according to the section parameters of the main beam; E=2.06×105N / mm is obtained according to the material type 2 , f y =345MPa; the ultimate plastic strain of materials commonly used in engineering at present ε u = 2.5%.
[0045] See attached figure 2 , according to the component performance index in the FEMA code, refer to FEMA-356 (Table 5-6), and determine the plastic rotation angle a when the component reaches the ultimate strength C is 4θ y , that is μ a for 4. According to the type of the member and the symmetry of the section, formula (III) is used to calculate the beam n =16.5, that is, the length of the plastic corner section 2 is 1 / 16.5 of the component length.
[0046] b. Form a fiber model for loading solution
[0047] See attached figure 1 , determine the distribution of fibers 11 on the fiber cross-section 10, use an e...
Embodiment 2
[0049] A steel column Z with a cross-section of 800×500×28×28 and a material strength of Q345 1 As an example, γ=1.22 is calculated according to the section parameters; E=2.06×105N / mm is obtained according to the material type 2 , f y =345MPa; material limit plastic strain ε u Take 2.5%; refer to FEMA-356 (Table 5-6) to determine the plastic rotation angle a when the member reaches the ultimate strength C is 4θ y , that is μ a for 4. According to the type of the member and the symmetry of the section, the formula (IV) is used to calculate the column n =19.3, that is, the length of the plastic corner section 2 is 1 / 19.3 of the component length.
[0050] b. Form a fiber model for loading solution
[0051] Carry out the loading solution in the same way as in step b of Example 1, so that the failure of the component in the numerical simulation during the dynamic response process meets both the deformation limit of the FEMA component and the strain limit of the material, and ...
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