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首页> 外文期刊>Journal of Spacecraft and Rockets >Characterization of Complex Porous Structures for Reusable Thermal Protection Systems: Porosity Measurements
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Characterization of Complex Porous Structures for Reusable Thermal Protection Systems: Porosity Measurements

机译:可重复使用的热防护系统的复杂多孔结构的表征:孔隙度测量

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摘要

This work is focused on the nonintrusive characterization of the local and average porosity of a prototype carbon-carbon nose, representative of a reusable thermal protection system based on transpiration cooling. A study based on the x-ray computed tomography scan of the specimen has been carried out with the purpose of defining the most important guidelines for the permeability tests, which are the minimum area to be probed with a hot-film anemometer and the correct distance of the mass flux sensor from the wall. The former has been calculated from the average porosity calculation, whereas the latter has been retrieved from the statistical analysis of the dimensions, and the distribution of the void structures inside the porous network coupled to the theory of fluid flow through perforated plates. Several longitudinal and transversal sectioning planes with respect to the symmetry axis of the carbon mask have been analyzed to calculate the internal porosity from the two-dimensional images, whereas the three-dimensional reconstruction of the sample has been used to retrieve the average volumetric porosity. Both the nominal values of the two-dimensional porosity and volumetric porosity have provided the same dimension of the characteristic area to be probed with a hot-film sensor for the permeability measurements. Preliminary permeability tests, performed within the predicted dimension of the control surface, have confirmed the uniformity of the mean velocity field and allowed verifying the range of variation of the correct distance of a hot-film sensor from the wall obtained from the statistical analysis of the computed tomography images.
机译:这项工作的重点是原型碳碳鼻的局部和平均孔隙度的非侵入性表征,代表了基于蒸腾冷却的可重复使用的热保护系统。进行了基于样本的X射线计算机断层扫描的研究,目的是确定渗透性测试的最重要准则,即使用热膜风速计探测的最小区域和正确的距离。壁上的质量通量传感器的角度。前者是根据平均孔隙率计算得出的,而后者是根据对尺寸的统计分析得出的,而多孔网络内部孔隙结构的分布与流体流过多孔板的理论相联系。分析了相对于碳掩模的对称轴的几个纵向和横向剖切面,以从二维图像计算内部孔隙率,而样品的三维重建已用于检索平均体积孔隙率。二维孔隙率和体积孔隙率的标称值都提供了要用热膜传感器探测的用于渗透率测量的特征区域的相同尺寸。在控制表面的预测尺寸内进行的初步渗透性测试已确认平均速度场的均匀性,并允许验证热膜传感器与壁之间的正确距离的变化范围,该范围是通过对壁的统计分析得出的计算机断层扫描图像。

著录项

  • 来源
    《Journal of Spacecraft and Rockets》 |2015年第1期|166-176|共11页
  • 作者单位

    Univ Texas Arlington, Aerosp Engn, Arlington, TX 76019 USA;

    Univ Texas Arlington, Aerosp Engn, Arlington, TX 76019 USA;

    Carbon Carbon Adv Technol Inc, Kennedale, TX 76060 USA;

    Carbon Carbon Adv Technol Inc, Kennedale, TX 76060 USA;

    Univ Texas Arlington, Aerosp Engn, Arlington, TX 76019 USA;

    Univ Texas Arlington, Mech & Aerosp Engn, Arlington, TX 76019 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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