HTPB固体推进剂的双轴拉伸力学性能

IF 1.1 4区 工程技术 Q3 ENGINEERING, AEROSPACE International Journal of Aerospace Engineering Pub Date : 2023-10-06 DOI:10.1155/2023/2407730
Li Jin, Qinzhi Fang, Xingwei Yan, Qinwei Hu
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引用次数: 0

摘要

研究了不同加载速率比和加载速度对端羟基聚丁二烯(HTPB)固体推进剂双轴张力的影响。设计并使用了一种合适的双轴拉伸试样,其中心部位的应力可以在每个加载方向上得到,并采用数字图像相关(DIC)方法得到其中心部位的应变。通过实验得到了各方向的应力应变关系。得到了单轴应力应变曲线和双轴应力应变曲线,发现加载速度对HTPB推进剂的双轴拉伸性能有显著影响。Mises等效应力应变可用于描述双轴拉伸应力应变状态,得到的指数本构模型可用于预测不同试验条件下的应力应变曲线。
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Biaxial Tensile Mechanical Properties of HTPB Solid Propellant
The purpose of this work is to study the effects of different loading rate ratios and loading speeds on the biaxial tension of hydroxyl-terminated polybutadiene (HTPB) solid propellant. A proper kind of biaxial tensile specimen with which the stresses in its central part can be obtained with the loads acted on each loading direction is designed and used in the study, and the strains in its central parts are obtained with the digital image correlation (DIC) method. The stress and strain relationship at each direction can be obtained by experiments. The uniaxial stress vs. strain curves and the biaxial stress vs. strain curves were obtained, and it was found that the loading speed remarkably influenced the biaxial tensile behaviors of HTPB propellant. The Mises equivalent stress and strain could be used to describe the biaxial tension stress and strain state, and the exponential constitutive model obtained in the study could be used to predict the stress vs. strain curve under different test conditions.
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来源期刊
CiteScore
2.70
自引率
7.10%
发文量
195
审稿时长
22 weeks
期刊介绍: International Journal of Aerospace Engineering aims to serve the international aerospace engineering community through dissemination of scientific knowledge on practical engineering and design methodologies pertaining to aircraft and space vehicles. Original unpublished manuscripts are solicited on all areas of aerospace engineering including but not limited to: -Mechanics of materials and structures- Aerodynamics and fluid mechanics- Dynamics and control- Aeroacoustics- Aeroelasticity- Propulsion and combustion- Avionics and systems- Flight simulation and mechanics- Unmanned air vehicles (UAVs). Review articles on any of the above topics are also welcome.
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