A Stress Analysis Method for Bi-axially Loaded Fastener Hole in Composite Laminate of Finite GeometrySource: Journal of Applied Mechanics:;1998:;volume( 065 ):;issue: 003::page 787Author:Y. Xiong
DOI: 10.1115/1.2789131Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A stress analysis method has been developed for a biaxially loaded fastener hole in a laminated plate of finite geometry. The method is based on a variational formulation involving complex variables. In this method, the equilibrium and compatibility equations are satisfied in the domain of the plate due to the employment of the complex stress potentials and all the boundary conditions are satisfied through a variational statement. Therefore, the requirement for finite width corrections in relatively large fastener hole cases is avoided. The method has been verified through comparison with finite element results.
keyword(s): Composite materials , Laminates , Fasteners , Stress analysis (Engineering) , Geometry , Finite element analysis , Boundary-value problems , Equations , Equilibrium (Physics) AND Stress ,
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| contributor author | Y. Xiong | |
| date accessioned | 2017-05-08T23:55:37Z | |
| date available | 2017-05-08T23:55:37Z | |
| date copyright | September, 1998 | |
| date issued | 1998 | |
| identifier issn | 0021-8936 | |
| identifier other | JAMCAV-26450#787_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/119879 | |
| description abstract | A stress analysis method has been developed for a biaxially loaded fastener hole in a laminated plate of finite geometry. The method is based on a variational formulation involving complex variables. In this method, the equilibrium and compatibility equations are satisfied in the domain of the plate due to the employment of the complex stress potentials and all the boundary conditions are satisfied through a variational statement. Therefore, the requirement for finite width corrections in relatively large fastener hole cases is avoided. The method has been verified through comparison with finite element results. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A Stress Analysis Method for Bi-axially Loaded Fastener Hole in Composite Laminate of Finite Geometry | |
| type | Journal Paper | |
| journal volume | 65 | |
| journal issue | 3 | |
| journal title | Journal of Applied Mechanics | |
| identifier doi | 10.1115/1.2789131 | |
| journal fristpage | 787 | |
| journal lastpage | 790 | |
| identifier eissn | 1528-9036 | |
| keywords | Composite materials | |
| keywords | Laminates | |
| keywords | Fasteners | |
| keywords | Stress analysis (Engineering) | |
| keywords | Geometry | |
| keywords | Finite element analysis | |
| keywords | Boundary-value problems | |
| keywords | Equations | |
| keywords | Equilibrium (Physics) AND Stress | |
| tree | Journal of Applied Mechanics:;1998:;volume( 065 ):;issue: 003 | |
| contenttype | Fulltext |