plane stress analysis
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Author(s):  
Masoud Forsat ◽  
Farayi Musharavati ◽  
Arameh Eyvazian ◽  
Murat Demiral ◽  
Afrasyab Khan ◽  
...  

2020 ◽  
pp. 83-107
Author(s):  
Y.K. Cheung ◽  
L.G. Tham

2020 ◽  
Vol 90 (6) ◽  
pp. 1363-1372 ◽  
Author(s):  
Shuang Wang ◽  
Hai-Bing Yang ◽  
Cunfa Gao ◽  
Zengtao Chen

2020 ◽  
Vol 300 ◽  
pp. 25-46
Author(s):  
Valérie Parry ◽  
Somrerk Chandra-ambhorn ◽  
Thanasak Nilsonthi ◽  
Muriel Braccini

The mechanical behaviour and adhesion properties of thermal oxide scales are key issues for steel processing and long-term durability. This chapter aims at taking up the various aspects to be considered for such studies. The first part is devoted to a description of the origin of stress and stress quantification. Then, description of mechanical failure and damaging patterns of thermal oxide scales will be given. Finally, definitions of adhesion energy as well as quantitative methods to measure adhesion energy will be proposed. An appendix describing the hypotheses and the constitutive equations for plane stress analysis, which suits to oxide scales, is also given The purpose is enriched by references in particular to Alain Galerie’s co-workers’ publications.


2019 ◽  
Vol 20 (02) ◽  
pp. 2050022 ◽  
Author(s):  
Balakrishna Adhikari ◽  
B. N. Singh

In this paper, the buckling response of laminated functionally-graded CNT-reinforced composite (FG-CNTRC) plate structure is predicted under various types of non-uniform edge compression loading. For the finite element (FE) discretization of the plate, a nine degree of freedom (DOFs)-type polynomial-based higher-order shear deformation theory (HSDT) is considered. The application of non-uniform edge load causes the in-plane stress distribution to be non-uniform. Hence, the in-plane stresses need to be evaluated prior to the buckling analysis. These in-plane stresses are calculated using the in-plane stress analysis method by FE approach or the in-plane elasticity approach. The differential equations are obtained by employing the Lagrange equation of motion and solved as a general eigenvalue problem, after the differential equations are converted into homogeneous equations by means of FE procedure. The accuracy and adaptability of the present model are validated by comparing the present result with the available literature. Further, the impact on the buckling response of the laminated FG-CNTRC plate is investigated by various parameters such as span thickness ratio, aspect ratio, various edge constraints, and different types of non-uniform edge load, CNT fiber gradation and temperature dependency material properties.


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