scholarly journals Large-area damage prediction system based on finite element method for risk assessment of seismic slope failure in mountains area

2008 ◽  
Vol 45 (3) ◽  
pp. 207-218 ◽  
Author(s):  
Akihiko WAKAI ◽  
Norihiro TANAKA ◽  
Shinro ABE ◽  
Hiroyuki YOSHIMATSU ◽  
Kousei YAMABE ◽  
...  
2019 ◽  
Vol 2019 ◽  
pp. 1-18 ◽  
Author(s):  
Chaowei Sun ◽  
Junrui Chai ◽  
Bin Ma ◽  
Tao Luo ◽  
Ying Gao ◽  
...  

This paper uses the modified strength reduction finite element method to propose stability charts for pseudostatic stability analysis of three-dimensional (3D) homogeneous soil slopes subjected to seismic excitation. These charts are developed in a wide range of input parameters for purely cohesive slopes and cohesive-frictional slopes, respectively. Effect of the horizontal seismic load is approximately considered using the quasistatic approach. The stability charts allow to determine the factor of safety without any iterative procedure and identify the corresponding critical slope failure mechanism. A slope example is employed to illustrate the application and reliability of these stability charts.


2003 ◽  
Vol 2003.56 (0) ◽  
pp. 277-278
Author(s):  
Taiyou TAKUMA ◽  
Hiroshi OKADA ◽  
Yasuyoshi FUKUI ◽  
Noriyoshi KUMAZAWA

Geo-Risk 2017 ◽  
2017 ◽  
Author(s):  
Te Xiao ◽  
Dian-Qing Li ◽  
Zi-Jun Cao ◽  
Siu-Kui Au ◽  
Xiao-Song Tang

2017 ◽  
Vol 61 (2) ◽  
pp. 115
Author(s):  
Mohamed Latrache ◽  
Mohamed Nadir Amrane

This paper presents a numerical study pertaining to on the active vibration control (AVC) of the 3-D rectangle simply supported plate bonded of the piezoelectric sensor/ actuator pairs. AVC is a large area of interest either in all sections of industry or in research. One way to control the vibration of dynamic systems is by using piezoelectric materials. A finite element method (FEM) analysis is used to model the dynamic behavior of the system. The frequencies of the isotropic pate and a smart structure are verified by the comparison between the analytical calculations and simulation. A LQR controller is designed based on the independent mode space control techniques to stifle the vibration of the system. The change in the sizes of the patches was a clear impact on the control results, and also in the values of the voltage in actuator. The results were established by simulating in ANSYS and MATLAB.


2007 ◽  
Vol 121-123 ◽  
pp. 649-652
Author(s):  
Ki Don Kim ◽  
Young Suk Sim ◽  
Jun Ho Jeong ◽  
Hyun Kee Sohn ◽  
Eung Sug Lee ◽  
...  

We investigated the non-uniformity of the residual layer thickness caused by wafer deformation in an experiment that examined different wafer thicknesses using UV-NIL with an element-wise patterned stamp (EPS). Experiments using the EPS were performed on an EVG®620-NIL. Severe deformation of the wafer served as an obstacle to the spread of resin drops, which caused non-uniformity of the residual layer thickness. We also simulated the imprint process using a simplified model and finite element method to analyze the non-uniformity.


2010 ◽  
Vol 26-28 ◽  
pp. 303-309
Author(s):  
Feng Liu ◽  
Zhong Bo Zhang ◽  
Wen Feng Qin

The original structure stress state of No. zero frame of TB200 aircraft is analyzed by finite element method. The stress and the reasons of the crack on the frame are determined. The numerical analysis results fit well with the actual damage of the frame, and the finite element analysis model is verified to be reliable. The stress state of the damaged frame structure is analyzed, which shows that the undamaged frame structure must be reinforced. The reinforce plan for the undamaged frame structure is given. The reinforced frame structure is analyzed by finite element method. The stress state and the residual strength of the reinforced frame structure are given. It is showed that the reinforce plan causes an obvious descent of the frame stress. The load is mainly distributed on the reinforcement of the No. zero frame. The residual static strength of the reinforced structure is higher than the original structure. The possible secondary damage position and mode of the reinforced structure are predicted.


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