单侧涂层浮空器蒙皮材料的近场动力学模型

Peridynamic model of unilateral coated envelope material for aerostatics

  • 摘要: 基于近场动力学方法,构建了浮空器蒙皮材料的近场模型。首先阐述了近场动力学的基本理论,表明了蒙皮材料的材料性质及结构。然后将蒙皮材料离散为空间上的质点,基于复合材料的近场模型,分析了编织条件下,质点本构力和应变能密度的组成,推导了质点间的本构力方程及近场参数。最后利用动力松弛法编程模拟了材料的力学性能。结果表明,在该近场模型下,蒙皮材料受力下的拉伸-应变曲线能与其他模拟结果相对应,并且材料的拉伸模量符合实验结果。

     

    Abstract: A peridynamic model for envelope material was established based on peridynamic theory. First, the basic theory of peridynamic and the major property of envelope material were illustrated. The material was scattered into particles, and based on a classic peridynamic model of composites, the components of constitutive force and strain energy density of each particle were analyzed under a unique condition of intertexture. The constitutive function and peridynamic parameter were divaricated thus completed the model. Emulation of mechanical property was conducted using dynamic relaxation method. The results show a correspondent stress state under tension with an alternative numerical result. The tensile modulus and the load-strain curve are in accordance with the lab results.

     

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