THE EFFECT OF THE ORIENTATION OF A CRACK ON THE CRITICAL BUCKLING LOAD IN A HYBRID COMPOSITE.

المؤلفون

  • N Hamani University Abdelhamid Ibn Badis of Mostaganem
  • D Ouinas University Abdelhamid Ibn Badis of Mostaganem

الكلمات المفتاحية:

buckling، hybrid composites، finite element analysis، crack

الملخص

In this work an analysis of buckling was carried out on rectangular plates hybrid composites with and without circular notch using the finite element method. The buckling strength of the laminated plate subjected to the uniaxial compression is highlighted according to the orientations of the fibers. The results show that increasing the thickness of the aluminum layer significantly improves the resistance to buckling. Whatever the orientation of the crack the critical buckling load remains stable.

السير الشخصية للمؤلفين

N Hamani، University Abdelhamid Ibn Badis of Mostaganem

LMNEPM, Department of Mechanics

D Ouinas، University Abdelhamid Ibn Badis of Mostaganem

LMNEPM, Department of Mechanics

المراجع

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N. Hamani, D. Ouinas, N. Benderdouche and M. Sahnoun. Buckling analyses of the antisymetrical composite laminate plate with a crack from circular notch. Advanced Materials Research.. (ISSN: 1022- 6680) vol.365 (2012) pp. 56-61, Trans Tech.Publications, Switzerland, on-line at www.scientifc.net.

التنزيلات

منشور

2016-06-01

كيفية الاقتباس

Hamani, N., & Ouinas, D. (2016). THE EFFECT OF THE ORIENTATION OF A CRACK ON THE CRITICAL BUCKLING LOAD IN A HYBRID COMPOSITE. مجلة علوم و تكنولوجيا ب، علوم الهندسة, (43), 17–22. استرجع في من https://revue.umc.edu.dz/b/article/view/2028

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