An improved higher order model for analysis of composite laminated cylindrical shell under thermal and electromechanical loads /
Modern aerospace structures are smart composite structures which are made from combination of composite and piezoelectric materials. These composite structures during their service life are exposed to severe environmental conditions such as high temperature and moisture effect that are detrimental t...
محفوظ في:
المؤلف الرئيسي: | Muhammad Rahman Adedi (مؤلف) |
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التنسيق: | أطروحة |
اللغة: | English |
منشور في: |
Kuala Lumpur :
Kulliyyah of Engineering, International Islamic University Malaysia,
2019
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الموضوعات: | |
الوصول للمادة أونلاين: | http://studentrepo.iium.edu.my/handle/123456789/5159 |
الوسوم: |
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مواد مشابهة
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An accurate model for analysis of composite laminated cylindrical shells under hygrothermal loads /
بواسطة: Al-Subari, Saleh Naji Musaed -
An improved zig-zag model for the mechanical behaviour of laminated composite curved beams and shells /
بواسطة: Xavier, Pascal B.
منشور في: (1994) -
Dynamic response of the pressurized laminated composite cylindrical shell subjected to impact loading
بواسطة: Firouzabadi, Farzin
منشور في: (2012) -
Free vibration analysis of laminated composite plates based on higher order shear deformation theory using finite element method /
بواسطة: Mohd Sultan Ibrahim
منشور في: (2002) -
Dynamic stability of cylindrical shells under periodic loading /
بواسطة: Ng, Teng Yong
منشور في: (1998)