Research on Fast Calculation of Rigid Plasticity Finite Element Method in Hot Strip Rolling

2008 ◽  
Vol 575-578 ◽  
pp. 288-292
Author(s):  
Chang Sheng Li ◽  
S.N. Song ◽  
R.B. Mei ◽  
G.L. Zhang ◽  
Xiang Hua Liu

Fast Finite Element (FFE) method had advantage of high precision and fast computing velocity. The online application of FFE method was significance both in theory and practice. In this paper the fast calculation of rigid plastic finite element method (RPFEM) in hot strip rolling was developed in this paper. The results of rolling force were good agreement to the measured results. The influence of element on calculating time and accuracy was discussed. The running time of one-dimension search was reduced greatly by combining Newton method with Brent method. Improved Newton method with trust region method and forced positive definite Hessian matrix method were used to reduce the convergence time. The better initial value could be obtained by improved mid-point integral Newton method. In addition, the influence of operating system, hardware and software on the calculating time was also discussed. The project of temperature FFE online calculation application in a plate mill was put forward.

2009 ◽  
Vol 209 (4) ◽  
pp. 1816-1825 ◽  
Author(s):  
G.L. Zhang ◽  
S.H. Zhang ◽  
J.S. Liu ◽  
H.Q. Zhang ◽  
C.S. Li ◽  
...  

2010 ◽  
Vol 46 (12) ◽  
pp. 1146-1154 ◽  
Author(s):  
S.H. Zhang ◽  
G.L. Zhang ◽  
J.S. Liu ◽  
C.S. Li ◽  
R.B. Mei

2020 ◽  
Vol 2020 ◽  
pp. 1-10
Author(s):  
Jianwei Li ◽  
Jinghua Wang ◽  
Leian Zhang ◽  
Xuemei Huang ◽  
Yongfeng Yu

Delamination is detrimental to the composite materials, and it may occur in the manufacturing process of the unidirectional laminate of the spar cap in wind turbine blades. This paper studies the effect of different delamination defects on the strength of the unidirectional laminate. The finite element model of laminate with different delamination areas and delamination heights is established using solid elements. The eigenvalues of laminates have different parameters calculated based on the finite element method. The final coupon test is used to verify the conclusions of simulation results. The finite element method presented in this study shows excellent capabilities to predict the buckling behavior of the laminate. The buckling eigenvalue of tested laminate is negatively correlated with the delamination area and positively correlated with the delamination height under the edgewise load. The S11, which is too high at the boundary of the delamination region, plays a significant role in buckling failure. It has a particular reference value for testing the laminate of blade both in theory and practice.


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