EXPERIMENTAL AND NUMERICAL STUDY OF THE BUCKLING OF SEMI-CYLINDRICAL COMPOSITE LATTICE

Q: How can I download an article?

To download an article from SID, first log in to the site, search for the article title, and click on the 'Download Article' option.

Q: How can I download an ISI article?

To download an ISI article on SID, enter the keyword or article title in the search bar, view the relevant results, click on the desired article, and select the 'Download Article' option.

Q: How can I access the SID database?

To access the SID database, visit SID.ir, create an account, and log in to access scientific resources.

Q: Is downloading articles from SID free?

Some articles on SID are available for free, while others require payment. Details are specified on the article's page.

KHALILI SEYED MOHAMMAD REZA; SEDIGH YASER; MIR MOHAMMAD HOSSEIN AHARI SEYED MAHYAR

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Journal Paper

Paper Information

Journal: Journal of Science and Technology of Composites Year:2016 | Volume:3 | Issue:3 Page(s): 269-276

Download Full-Text

Persian Verion

View:

955

Download:

Cites:

Information Journal Paper

Title

EXPERIMENTAL AND NUMERICAL STUDY OF THE BUCKLING OF SEMI-CYLINDRICAL COMPOSITE LATTICE

Author(s)

KHALILI SEYED MOHAMMAD REZA | SEDIGH YASER | MIR MOHAMMAD HOSSEIN AHARI SEYED MAHYAR | Issue Writer Certificate

Keywords

COMPOSITEQ2

SEMI-CYLINDRICAL LATTICEQ2

RIBQ2

BUCKLINGQ2

Abstract

COMPOSITE lattice structures, due to their advantages such as high strength, light weight and resistance to corrosion are recently employed in various industrial applications including aerospace and marine structures. These structures are usually composed of two major parts: the shell and the lattice structure.The lattice part is made of a system of Helical, Hoop or axial RIBs. During loading, the loads are transferred to the RIBs and the RIBs distribute the loads throughout the structure. In the present paper, first the fabrication of the SEMI-CYLINDRICAL LATTICE structure is explained. Then, the BUCKLING behavior of the semicylindrical lattice structure is investigated using the ABAQUS finite element software. The effect of various parameters such as the thickness and ply angles in the shell laminate were studied. Moreover, the effect of RIB parameters such as different patterns and the RIB thicknesses were obtained by finite element analysis.In addition, in order to validate the results, a comparison between the experimental and finite element results was performed.

Cites

No record.

References

No record.

Cite

APA: Copy

KHALILI, SEYED MOHAMMAD REZA, SEDIGH, YASER, & MIR MOHAMMAD HOSSEIN AHARI, SEYED MAHYAR. (2016). EXPERIMENTAL AND NUMERICAL STUDY OF THE BUCKLING OF SEMI-CYLINDRICAL COMPOSITE LATTICE. JOURNAL OF SCIENCE AND TECHNOLOGY OF COMPOSITES (JSTC), 3(3), 269-276. SID. https://sid.ir/paper/251637/en

Vancouver: Copy

KHALILI SEYED MOHAMMAD REZA, SEDIGH YASER, MIR MOHAMMAD HOSSEIN AHARI SEYED MAHYAR. EXPERIMENTAL AND NUMERICAL STUDY OF THE BUCKLING OF SEMI-CYLINDRICAL COMPOSITE LATTICE. JOURNAL OF SCIENCE AND TECHNOLOGY OF COMPOSITES (JSTC)[Internet]. 2016;3(3):269-276. Available from: https://sid.ir/paper/251637/en

IEEE: Copy

SEYED MOHAMMAD REZA KHALILI, YASER SEDIGH, and SEYED MAHYAR MIR MOHAMMAD HOSSEIN AHARI, “EXPERIMENTAL AND NUMERICAL STUDY OF THE BUCKLING OF SEMI-CYLINDRICAL COMPOSITE LATTICE,” JOURNAL OF SCIENCE AND TECHNOLOGY OF COMPOSITES (JSTC), vol. 3, no. 3, pp. 269–276, 2016, [Online]. Available: https://sid.ir/paper/251637/en

Related Journal Papers