کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
6748490 | 1430175 | 2018 | 54 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Buckling of quasi-perfect cylindrical shell under axial compression: A combined experimental and numerical investigation
ترجمه فارسی عنوان
خم کردن پوسته استوانه ای شبه مطلوب تحت فشرده سازی محوری: یک بررسی ترکیبی تجربی و عددی
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مهندسی عمران و سازه
چکیده انگلیسی
Imperfections from manufacturing process can cause a scattered reduction of the load-carrying capacity or buckling load of axially compressed cylindrical shell structures. To isolate the influence of geometric imperfections from other imperfections such as welding, a sub-scaled, integrally manufactured cylindrical shell with small-amplitude geometric imperfection was manufactured, analyzed and tested in this study. A test facility and measurement system (including imperfection measurement and buckling test) were constructed. Finite element (FA) numerical procedure for predicting the buckling load was developed. Results indicate that the buckling load predicted by the FE analysis is very close to that from the test. Knockdown factor (KDF) is discussed with reference to the NASA design document. Furthermore, the influence of pure geometric imperfections including imperfection component and amplitude on the buckling behavior is discussed based on Fourier series method. Some guidance for the dimensional tolerance in manufacturing process relating to the load-carrying capacity of thin-walled structures is provided.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: International Journal of Solids and Structures - Volumes 130â131, January 2018, Pages 232-247
Journal: International Journal of Solids and Structures - Volumes 130â131, January 2018, Pages 232-247
نویسندگان
Wang Bo, Zhu Shiyang, Hao Peng, Bi Xiangju, Du Kaifan, Chen Bingquan, Ma Xiangtao, Chao Yuh J.,