Application of fractional calculus methods to viscoelastic behaviours of solid propellants

Author:

Fang Changqing1,Shen Xiaoyin1,He Kuai1,Yin Chao1,Li Shasha1,Chen Xiaolong1,Sun Huiyu2ORCID

Affiliation:

1. Shanghai Space Propulsion Technology Research Institute, 1777 Zhongchun Rd, Shanghai 201109, People's Republic of China

2. 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

Abstract

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'.

Publisher

The Royal Society

Subject

General Physics and Astronomy,General Engineering,General Mathematics

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