在动态条件下的喷气式飞机目标背后的参数预测方法研究
Xuepeng Zhang1, Can Xu2, Yizhen Wang1
1School of Mechanical and Electrical Engineering, North University of China, Taiyuan, 030051, Shanxi, China.
Scientific reports
|November 25, 2025
概括
这项研究模拟了电荷喷射穿透的形状,揭示了侧向干扰如何影响剩余速度和直径. 这些发现提供了一种验证的方法,用于在动态情况下评估目标后的性能.
科学领域:
- 固体力学 固体力学是什么
- 计算流体动力学的流体动力学.
- 材料科学 材料科学 材料科学
背景情况:
- 对动态场景来说,了解目标撞击后的形状充电喷气行为至关重要.
- 现有的模型往往缺乏在干扰下对目标后喷气演变的全面描述.
研究的目的:
- 在动态条件下系统地描述形状的充电喷气在目标后的行为.
- 开发一个预测模型,用于喷气的残速和后目标直径,考虑到横向扰动.
主要方法:
- 建立一个有限元模型,用于通过有限厚度的移动目标穿透喷气.
- 整合虚拟起源理论和维度分析,引入一个虚拟源参数.
- 通过静态和动态透实验验验证的工程预测模型的开发.
主要成果:
- 剩余喷气速度随着横向干扰的增加而呈指数级下降.
- 目标后喷气直径表现出具有横向干扰的指数增长.
- 数字预测,模型输出和实验数据显示出强烈的一致性.
结论:
- 拟议的有限元模型和工程预测模型准确地描述了目标喷气后的行为.
- 提供了一种经过验证的方法来评估动态场景中的成型电荷目标后性能.
- 虚拟源参数有效量化目标后喷气指标.
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