摘要:
富燃料炸药在封闭空间内发生爆炸时,其载荷形态相较于开放空间差异显著,反射冲击波大幅增强,燃热耦合效应显著,内爆载荷作用下结构变形计算涉及变量多、形式复杂、研究成本高。针对上述问题,本文基于经验证的封闭空间内考虑燃热增强效应的爆炸载荷数值计算方法,系统分析了封闭空间内爆炸载荷的时空分布规律,并提出一种同时考虑饱和响应时间与准静态压力的等效载荷简化方法。通过研究等效载荷空间分布形式及准静态压力对结构响应的影响,结果表明:在当前研究范围内,等效载荷空间分布对结构响应的影响相对较小,而准静态压力贡献不可忽略。根据上述认识,进一步提出了基于靶板中心点载荷特性的两阶段载荷简化模型,经过对比10组简化模型与试验的残余变形值,验证了简化模型的有效性。研究表明,该模型在不同工况下均具有良好的适用性,能够在保证计算精度的同时显著提升计算效率,可为封闭空间爆炸相关工程问题的简化分析提供技术路径。
Abstract:
When fuel-rich explosives are detonated in a confined space, their load characteristics are verified to exhibit remarkable differences from those generated in an open space. Specifically, the reflected shock waves are significantly intensified, the afterburning effect is prominently manifested, and the effective duration during which the expansion of detonation products performs work is obviously prolonged. Meanwhile, the calculation of structural deformation under the action of confined blast loading is confronted with multiple challenges, including a large number of involved variables, complex expression forms and high research costs. To tackle these problems, based on a validated numerical calculation method for explosion loads in confined spaces where the afterburning effect is taken into consideration, a systematic analysis is carried out on the spatiotemporal distribution law of explosion loads in confined spaces, and an equivalent load simplification method that simultaneously accounts for the saturation response time and quasi-static pressure is proposed in this paper. Through an in-depth investigation into the spatial distribution form of the equivalent load and the influence exerted by quasi-static pressure on structural response, the results demonstrate that within the scope of the current research, the impact of the spatial distribution of the equivalent load on structural response is relatively minor, whereas the contribution of quasi-static pressure cannot be neglected. On the basis of the above research findings, a two-stage load simplification model represented by the load characteristics at the central point of the target plate is further developed. A comparative analysis is conducted between the residual deformation values derived from 10 groups of simplified models and those obtained from actual experiments, which verifies the effectiveness of the established simplified model. The research results indicate that the proposed model possesses excellent applicability under different working conditions, can not only guarantee calculation precision but also remarkably enhance computational efficiency, and thus provides a reliable technical approach for the simplified analysis of engineering problems related to confined space explosions.