A Gridless Method for Computing Interior Ballistic Flows With Moving Discrete Points

IF 2.1 4区 工程技术 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS
Shubham K. Vyas, Jayachandran T, Mathur Girijesh, Rajesh G
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引用次数: 0

Abstract

This study presents a meshless computational framework for simulating unsteady fluid dynamics in interior ballistic applications. The proposed meshless method eliminates the need for grid generation and deformation by utilizing a cloud of dynamically moving points, based on the Arbitrary Lagrangian–Eulerian (ALE) formulation. The key novelty of this work is integrating the meshless solver with a moving points system, which makes it highly suitable for ballistics applications involving complex geometries. Furthermore, the combustion process has been simplified, streamlining the simulation by avoiding the need for fully modeling propellant combustion, as required in multiphase solvers. The framework discretizes the unsteady axisymmetric Euler equations using local weighted least-squares approximations to calculate derivatives. Numerical fluxes are computed using a modified Harten, Lax, van Leer, Contact (HLLC) scheme, which is essential for achieving high accuracy and effectively capturing complex flow features. Temporal evolution is handled using the Explicit Strong Stability Preserving (ESSP) Runge–Kutta method, ensuring stability and accuracy under unsteady flow conditions. The method is applied to interior ballistic simulations, such as the motion of an M107–155 mm shell launched through an M185 cannon, achieving excellent agreement with experimental observations, particularly in predicting muzzle velocity and peak pressure. The simplified setup of this framework enables it to handle large grid deformations and complex geometries, and makes it an efficient, high-fidelity solution for dynamic flow problems in ballistics and aerospace, serving as a reliable predictive and assessment tool for interior ballistics studies. Further, the pressure wave analysis conducted within this framework provides valuable insights for optimizing shell design and propellant combustion characteristics, while also enhancing its role as a predictive tool for assessing shell integrity and mitigating resonance-induced structural risks in interior ballistics applications.

运动离散点弹道内流的无网格计算方法
本文提出了一种用于内弹道非定常流体动力学模拟的无网格计算框架。提出的无网格方法基于任意拉格朗日-欧拉(ALE)公式,利用动态移动的点云,消除了网格生成和变形的需要。这项工作的关键新颖之处在于将无网格求解器与移动点系统集成在一起,这使得它非常适合涉及复杂几何形状的弹道应用。此外,燃烧过程也得到了简化,避免了像多相求解器那样需要对推进剂燃烧进行完全建模,从而简化了模拟过程。该框架采用局部加权最小二乘近似对非定常轴对称欧拉方程进行离散化计算导数。数值通量的计算采用改进的Harten, Lax, van Leer, Contact (HLLC)格式,该格式对于实现高精度和有效捕获复杂的流动特征至关重要。时间演化采用显式强稳定保持(ESSP)龙格-库塔方法处理,保证了非定常流条件下的稳定性和准确性。将该方法应用于内弹道仿真,如M107-155毫米炮弹通过M185火炮发射的运动,与实验观测结果非常吻合,特别是在预测初速和峰值压力方面。该框架的简化设置使其能够处理大网格变形和复杂几何形状,并使其成为弹道和航空航天中动态流动问题的高效,高保真解决方案,可作为内弹道研究的可靠预测和评估工具。此外,在此框架内进行的压力波分析为优化壳体设计和推进剂燃烧特性提供了有价值的见解,同时也增强了其作为评估壳体完整性和减轻内弹道应用中共振引起的结构风险的预测工具的作用。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
International Journal for Numerical Methods in Fluids
International Journal for Numerical Methods in Fluids 物理-计算机:跨学科应用
CiteScore
3.70
自引率
5.60%
发文量
111
审稿时长
8 months
期刊介绍: The International Journal for Numerical Methods in Fluids publishes refereed papers describing significant developments in computational methods that are applicable to scientific and engineering problems in fluid mechanics, fluid dynamics, micro and bio fluidics, and fluid-structure interaction. Numerical methods for solving ancillary equations, such as transport and advection and diffusion, are also relevant. The Editors encourage contributions in the areas of multi-physics, multi-disciplinary and multi-scale problems involving fluid subsystems, verification and validation, uncertainty quantification, and model reduction. Numerical examples that illustrate the described methods or their accuracy are in general expected. Discussions of papers already in print are also considered. However, papers dealing strictly with applications of existing methods or dealing with areas of research that are not deemed to be cutting edge by the Editors will not be considered for review. The journal publishes full-length papers, which should normally be less than 25 journal pages in length. Two-part papers are discouraged unless considered necessary by the Editors.
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