کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
6704351 1428520 2018 27 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Design-oriented crushing analysis of hexagonal honeycomb core under in-plane compression
ترجمه فارسی عنوان
تجزیه و تحلیل خرد کردن طراحی شده از هسته لانه زنبوری شش ضلعی تحت فشرده سازی در هواپیما
کلمات کلیدی
فشرده سازی درون هواپیما، لانه زنبوری شش ضلعی، فرایند تغییر شکل مالکیت فلات، جذب انرژی، روش عنصر محدود
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی عمران و سازه
چکیده انگلیسی
The square honeycomb core is compressed quasi-statically and dynamically in order to investigate the mechanical properties of it. The plastic collapse stress under static compression is mathematically discussed by investigating the collapse mechanisms of cells from numerical simulations. Results show that the plastic collapse stress in the y direction is larger than that in the x direction under multi-cell condition, which agrees with the conclusion of numerical simulations. This difference is insensitive to the relative density within a specific range under quasi-static compression. However, it turns to be insignificant when the crushing velocity reaches or exceeds a critical velocity. A reverse method is proposed to estimate this critical velocity. For the equi-biaxial compression analysis, deformation process of the honeycomb is defined to three modes, and the deformation map is drawn. Compared with true stresses in both x and y directions in uniaxial compression, performances of them in equi-biaxial compression are reinforced. To represent the true stress in mathematical way, empirical formula for high velocity compression is derived. The energy absorption capacity is also enhanced, and the process is smoother around the stage of full densification than that under uniaxial compression.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Composite Structures - Volume 187, 1 March 2018, Pages 429-438
نویسندگان
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