The stress intensity factors are calculated for a cracked sheet and cracked stiffeners attached with rivets. The approach adopted is based on compatibility of displacements among the sheet, fasteners, and stiffeners. Displacements in the cracked stiffener are determined by adding the induced displacements from cracks to intact stiffener displacements, which are obtained using empirical stress intensity equations. In addition, displacements in the cracked sheet are calculated using the basic solution of a single stiffener for analyzing any combinations of stiffener (either intact, broken, or cracked). Bending flexibilities of the sheet and stiffeners are ignored, and the analysis is conducted within the limitations of elasticity theory. The proposed method is verified by comparing it to numerically computed results from finite element analysis.
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January 1991
Research Papers
Stress Intensity Factors for a Cracked Stiffened Sheet With Cracked Stiffeners
T. Nishimura
T. Nishimura
Mitsubishi Heavy Industries, Ltd., Nagoya Aerospace Systems Works, Nagoya, Japan
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T. Nishimura
Mitsubishi Heavy Industries, Ltd., Nagoya Aerospace Systems Works, Nagoya, Japan
J. Eng. Mater. Technol. Jan 1991, 113(1): 119-124 (6 pages)
Published Online: January 1, 1991
Article history
Received:
October 5, 1989
Revised:
March 5, 1990
Online:
April 29, 2008
Citation
Nishimura, T. (January 1, 1991). "Stress Intensity Factors for a Cracked Stiffened Sheet With Cracked Stiffeners." ASME. J. Eng. Mater. Technol. January 1991; 113(1): 119–124. https://doi.org/10.1115/1.2903366
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