首页> 外文学位 >Proximal bodies in hypersonic flow.
【24h】

Proximal bodies in hypersonic flow.

机译:高超声速流中的近身。

获取原文
获取原文并翻译 | 示例

摘要

The problem of proximal bodies in hypersonic flow is encountered in several important situations, both natural and man-made. The present work seeks to investigate one aspect of this problem by exploring the forces experienced by a secondary body when some part of it is within the shocked region created by a primary body travelling at hypersonic speeds.; An analytical methodology based on the blast wave analogy is developed and used to predict the secondary force coefficients for simple geometries in both two and three dimensions. When the secondary body is entirely inside the primary shocked region, the nature of the lateral coefficient is found to depend strongly on the relative size of the two bodies. For two spheres, the methodology predicts that the secondary body will experience an exclusively attractive lateral force if the secondary diameter is larger then one-sixth the primary diameter. The analytical results are compared with numerical simulations carried out using the AMROC software and good agreement is obtained if an appropriate normalization for the lateral displacement is used.; Results from a series of experiments in the T5 hypervelocity shock tunnel are also presented and compared with perfect-gas numerical simulations, again with good agreement. In order to model this situation experimentally, a new force-measurement technique for short-duration hypersonic facilities has been developed, and results from the validation experiments are included.; Finally, the analytical methodology is used to model two physical situations. First, the entry of a binary asteroid system into the Earth's atmosphere is simulated. Second, a model for a fragmenting meteoroid in a planetary atmosphere is developed, and simulations are carried out to determine whether the secondary scatter patterns in the Sikhote-Alin crater field may be attributed to aerodynamic interactions between fragments rather than to secondary fragmentation. It is found that while aerodynamic interactions lead to increased secondary crater grouping, these groups do not exhibit the typically elliptical shape that we would expect secondary fragmentation to produce.
机译:在自然和人为的几种重要情况下,都会遇到高超声速流动中近端物体的问题。本工作试图通过探索次要物体的一部分处于处于以超音速运动的主要物体产生的冲击区域内时所经历的力,来研究这一问题的一个方面。开发了一种基于爆炸波类比的分析方法,并将其用于预测二维和三维中简单几何形状的次级力系数。当次要主体完全位于主要受激区域内时,发现横向系数的性质在很大程度上取决于两个主体的相对大小。对于两个球体,该方法预测,如果次级直径大于初级直径的六分之一,则次级物体将承受排他性的吸引力。将分析结果与使用AMROC软件进行的数值模拟进行比较,如果对横向位移使用了适当的归一化,则可以获得良好的一致性。还介绍了T5超高速冲击隧道中的一系列实验结果,并将其与完美气体数值模拟进行了比较,再次具有很好的一致性。为了通过实验对这种情况进行建模,已经开发了一种用于短时高超音速设施的新型测力技术,并包括了验证实验的结果。最后,分析方法用于对两种物理情况进行建模。首先,模拟了一个双星小行星系统进入地球大气层的过程。其次,开发了一种在行星大气中分裂流星体的模型,并进行了模拟以确定Sikhote-Alin陨石坑场中的次级散射模式是否可归因于碎片之间的空气动力学相互作用,而不是归因于次级碎片。已发现,尽管空气动力学相互作用导致次级陨石坑的分组增加,但这些分组并没有表现出我们期望产生次级碎裂的典型椭圆形状。

著录项

  • 作者

    Laurence, Stuart J.;

  • 作者单位

    California Institute of Technology.;

  • 授予单位 California Institute of Technology.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2006
  • 页码 192 p.
  • 总页数 192
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索 ;
  • 关键词

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号