基于分数阶Maxwell模型的NEPE推进剂宽泛应变率力学行为研究OA
Mechanical behavior of NEPE propellant at a wide range of strain rates based on the fractional-order Maxwell model
针对固体推进剂在宽泛应变率下表现出的不同力学响应,采用分数阶算子的 Grünwald-Letnikov 定义推导了三维分数阶 Maxwell 本构模型及其差分迭代格式,研究了分数阶黏弹性模型描述宽泛应变率下 NEPE 推进剂本构关系的能力.基于 NEPE 推进剂材料的霍普金森压杆试验及高速拉伸试验数据,采用遗传算法对分数阶本构模型中的参数进行识别,并利用 3 500、4 100、4 600 s-1 应变率下的试验数据对分数阶 Maxwell 本构模型进行验证.结果表明,该本构模型表现出强率相关性,对于高中低三种不同应变率,可分别用 1 组参数表征多组应变率下的黏弹性力学行为,全时程试验值与解析解的相对误差基本小于 20%,解析解与有限元数值解的相对误差均小于 2%,验证了三维分数阶 Maxwell 模型描述不同应变率下 NEPE 推进剂力学行为的可行性和准确性.
In view of the distinct mechanical responses exhibited by solid propellants across a wide range of strain rates,the three-dimensional fractional-order Maxwell constitutive model and its difference iterative scheme were derived by using the Grünwald-Letnikov definition of the fractional-order operator.The ability of the fractional-order viscoelastic model to characterize the constitutive relationship of NEPE propellants under a wide range of strain rates was systematically investigated.Based on the Split Hopkinson pressure bar tests and high-speed tensile experimental data of NEPE propellants,the parameters of the fractional Maxwell constitutive model were identified using a genetic algorithm,and the fractional Maxwell constitutive model was verified using the test data at strain rates of 3 500 s-1,4 100 s-1 and 4 600 s-1.The results demonstrate that this constitutive model exhibits a strong rate dependence.For the high,medium and low strain rates,the viscoelastic mechanical behavior under multiple strain rates can be well characterized by a set of parameters respectively.The relative errors between the full-duration experimental values and the analytical solutions are basically less than 20%,while those between the analytical solutions and finite element numerical solutions are less than 2%.This validates the feasibility and accuracy of the three-dimensional fractional-order Maxwell model in describing the mechanical behaviors of NEPE propellants over a wide range of strain rates.
王新彤;任全彬;何高让;郜婕;梁渊哲
西安航天动力技术研究所,西安 710025航天动力技术研究院,西安 710025西安航天动力技术研究所,西安 710025西安航天动力技术研究所,西安 710025西安航天动力技术研究所,西安 710025
航空航天
分数阶Maxwell模型NEPE推进剂宽泛应变率遗传算法
fractional-order Maxwell modelNEPE propellantwide range of strain ratesgenetic-algorithm
《固体火箭技术》 2026 (2)
249-259,11
国家级项目.
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