OPTIMAL SHAPE FOR THE UNSYMMETRIC BONDED COMPOSITE REPAIR

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KOUCHAKZADEH M.A.; GHANATI P.

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Journal: MECHANICAL ENGINEERING SHARIF (SHARIF: MECHANICAL ENGINEERING) Year:2005 | Volume:21 | Issue:31 Page(s): 57-63

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Title

OPTIMAL SHAPE FOR THE UNSYMMETRIC BONDED COMPOSITE REPAIR

Author(s)

KOUCHAKZADEH M.A. | GHANATI P. | Issue Writer Certificate

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Abstract

The bonded repair of cracked metallic plates of airplanes with composite materials has proved to be highly effective, due to high strength, low weight and easy application. Here a center cracked aluminum plate with an unsymmetric bonded composite repair patch is considered and searched for optimum patch shape, using the two dimensional finite element method. The three layer technique is used in the model and the stress intensity factor is obtained from the modified crack closure method. Many patches with constant volume and different shape, including rectangular, elliptical and polygonal shapes, are investigated. The results show that the polygonal shape results in the lowest stress intensity factors.

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APA: Copy

KOUCHAKZADEH, M.A., & GHANATI, P.. (2005). OPTIMAL SHAPE FOR THE UNSYMMETRIC BONDED COMPOSITE REPAIR. MECHANICAL ENGINEERING SHARIF (SHARIF: MECHANICAL ENGINEERING), 21(31), 57-63. SID. https://sid.ir/paper/128266/en

Vancouver: Copy

KOUCHAKZADEH M.A., GHANATI P.. OPTIMAL SHAPE FOR THE UNSYMMETRIC BONDED COMPOSITE REPAIR. MECHANICAL ENGINEERING SHARIF (SHARIF: MECHANICAL ENGINEERING)[Internet]. 2005;21(31):57-63. Available from: https://sid.ir/paper/128266/en

IEEE: Copy

M.A. KOUCHAKZADEH, and P. GHANATI, “OPTIMAL SHAPE FOR THE UNSYMMETRIC BONDED COMPOSITE REPAIR,” MECHANICAL ENGINEERING SHARIF (SHARIF: MECHANICAL ENGINEERING), vol. 21, no. 31, pp. 57–63, 2005, [Online]. Available: https://sid.ir/paper/128266/en

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