کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
251116 502921 2015 8 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Strain rate effect on the out-of-plane dynamic compressive behavior of metallic honeycombs: Experiment and theory
ترجمه فارسی عنوان
تأثیر نرخ تنش بر رفتار فشاری دینامیکی خارج از لانه هلی کوپترهای فلزی: آزمایش و تئوری
کلمات کلیدی
لانه زنبوری فلزی، فشرده سازی پویا، اثر نرخ فشار، اثر اینرسی، استرس فلات
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی عمران و سازه
چکیده انگلیسی

Many studies reveal that the dynamic compressive strength of metallic honeycombs is higher than the quasi-static one, but the reasons for that are still debatable. This paper aims to study the strain rate effect of parent materials on the out-of-plane dynamic compressive behavior of metallic honeycombs. Quasi-static and dynamic tests on aluminum honeycombs were performed with universal testing machine and Split Hopkinson Pressure Bar, respectively. The velocity values of dynamic tests were from about 6 to 19 m/s. The present and existing measures of plateau stress are evaluated by both the rate-independent (R-I) and rate-dependent (R-D) shock theories. It is shown that the R-D shock theory proposed in our previous study provides more accurate predictions at low, medium and high impact velocities. Based on the R-D shock theory, the influences of strain rate effect are analyzed quantitatively and the change tendencies of measured plateau stresses with impact velocities are explained reasonably. The analysis indicates that the strain rate effect has a large contribution to the dynamic enhancement of metallic honeycombs in a wide velocity range.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Composite Structures - Volume 132, 15 November 2015, Pages 644–651
نویسندگان
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