Henry Michael M, Thomas Stephen, Alberts Mone't, Estridge Carla E, Farmer Brittan, McNair Olivia, Jankowski Eric
Micron School of Materials Science and Engineering, Boise State University, Boise, ID 83725, USA.
The Boeing Company, St. Louis, MO 63134, USA.
Polymers (Basel). 2020 Oct 30;12(11):2547. doi: 10.3390/polym12112547.
The objective of this work is to predict the morphology and material properties of crosslinking polymers used in aerospace applications. We extend the open-source dybond plugin for HOOMD-Blue to implement a new coarse-grained model of reacting epoxy thermosets and use the 44DDS/DGEBA/PES system as a case study for calibration and validation. We parameterize the coarse-grained model from atomistic solubility data, calibrate reaction dynamics against experiments, and check for size-dependent artifacts. We validate model predictions by comparing glass transition temperatures measurements at arbitrary degree of cure, gel-points, and morphology predictions against experiments. We demonstrate for the first time in molecular simulations the cure-path dependence of toughened thermoset morphologies.
这项工作的目标是预测用于航空航天应用的交联聚合物的形态和材料性能。我们扩展了用于HOOMD-Blue的开源dybond插件,以实现一种新的反应性环氧热固性材料的粗粒度模型,并将44DDS/DGEBA/PES系统作为校准和验证的案例研究。我们根据原子溶解度数据对粗粒度模型进行参数化,针对实验校准反应动力学,并检查尺寸相关的伪影。我们通过比较任意固化度下的玻璃化转变温度测量值、凝胶点以及与实验的形态预测来验证模型预测。我们首次在分子模拟中证明了增韧热固性材料形态的固化路径依赖性。