کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
6778671 1432068 2018 9 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
The in-plane effective length of members in aluminum alloy reticulated shell with gusset joints
ترجمه فارسی عنوان
طول مؤثر در هواپیما در پوسته بافته شده با آلومینیوم با مفاصل گسست
کلمات کلیدی
آلیاژ آلومینیوم، مفصل نیمه جامد، طول موثر، ثبات در هواپیما،
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی عمران و سازه
چکیده انگلیسی
This paper presents an analytical research on the in-plane stability of members in single-layer reticulated latticed shells with aluminum alloy gusset (AAG) joints. The influence of two kinds of actual boundary conditions are considered, namely, the stiffness of the AAG joint (k1) and restraint of adjacent members (k2). In order to explore the influence of k1, an experimental program including 5 member specimens with AAG joints is introduced, and finite element (FE) models are established and verified. Based on the test and FE results, the effective length of the specimens are obtained. Subsequently, theoretical analysis is conducted to investigate the effect of k2, with accounting for the stiffness reduction caused by axial compressive force. Finally, the effective length factors of members in reticulated shell with AAG joints are derived and tabulated. Numerical examples are presented to illustrate the necessity of considering the influence of k1 and k2, and verify the good accuracy of the given effective length factors.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Thin-Walled Structures - Volume 123, February 2018, Pages 483-491
نویسندگان
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