Fang Changqing, Shen Xiaoyin, He Kuai, Yin Chao, Li Shasha, Chen Xiaolong, Sun Huiyu
Shanghai Space Propulsion Technology Research Institute, 1777 Zhongchun Rd, Shanghai 201109, People's Republic of China.
State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, 29 Yudao Street, Nanjing 210016, People's Republic of China.
Philos Trans A Math Phys Eng Sci. 2020 May 29;378(2172):20190291. doi: 10.1098/rsta.2019.0291. Epub 2020 May 11.
A three-branch viscoelastic model based on fractional derivatives is proposed for the viscoelastic behaviours of solid propellants. The simulation results show a satisfactory agreement with the stress relaxation modulus and complex modulus of solid propellants. As a comparison, the static modulus is also characterized by traditional viscoelastic model with integer-order derivatives. Results show that the application of the fractional derivatives to the viscoelastic constitutive model can effectively reduce the number of the required parameters while giving an accurate prediction of viscoelastic behaviours of solid propellants. Moreover, a simple and effective direct search method based on simulated annealing and Powell's mothed is proposed for the data fitting. This article is part of the theme issue 'Advanced materials modelling via fractional calculus: challenges and perspectives'.
针对固体推进剂的粘弹性行为,提出了一种基于分数阶导数的三分支粘弹性模型。模拟结果表明,该模型与固体推进剂的应力松弛模量和复模量具有良好的一致性。作为对比,还采用具有整数阶导数的传统粘弹性模型对静态模量进行了表征。结果表明,将分数阶导数应用于粘弹性本构模型,在准确预测固体推进剂粘弹性行为的同时,能够有效减少所需参数的数量。此外,还提出了一种基于模拟退火和鲍威尔方法的简单有效的直接搜索方法用于数据拟合。本文是主题为“通过分数阶微积分进行先进材料建模:挑战与展望”的一部分。