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A8 POSTFLIGHT SUMMARY OF THE CAPILLARY FLOW EXPERIMENTS ABOARD THE INTERNATIONAL SPACE STATION

机译:A8国际空间站上的毛细管流动实验的飞行后总结

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This paper provides a summary of the experimental, analytical, and numerical results of the Capillary Flow Experiment (CFE) performed aboard International Space Station (ISS) from Increment 9 (beginning August, 2004) through Increment 16 (ending December, 2007), with 19 operations by 7 astronauts including: M. Fincke, W. McArthur, J. Williams, S. Williams, M. Lopez-Alegria, C. Anderson, and P. Whitson. CFE consists of 6 approximately 1 to 2kg experiment units designed to probe certain capillary phenomena of fundamental and applied importance, such as capillary flow in complex containers, critical wetting in discontinuous structures, and large length scale contact line dynamics. Highly quantitative video images from the simply performed flight experiments provide immediate confirmation of the usefulness of current analytical design tools, as well as provide guidance to the development of new ones. A brief review of the experiments and procedures is provided before reporting a selection of experimental results and comparisons with both analytic and numerical predictions. The products of the work include design tools for modeling capillary interface dynamics relevant to spacecraft engineering systems.
机译:本文总结了国际空间站(ISS)从增量9(从2004年8月开始)到增量16(从2007年12月开始)进行的毛细管流动实验(CFE)的实验,分析和数值结果,以及由7名宇航员进行的19项操作包括:M. Fincke,W. McArthur,J. Williams,S. Williams,M. Lopez-Alegria,C. Anderson和P. Whitson。 CFE由6个大约1到2kg的实验单元组成,旨在探测某些具有根本和应用重要性的毛细管现象,例如复杂容器中的毛细管流动,不连续结构中的临界润湿以及较大长度的接触线动力学。通过简单的飞行实验获得的高度定量的视频图像可立即确认当前分析设计工具的有用性,并为开发新工具提供指导。在报告实验结果的选择以及与分析和数值预测的比较之前,对实验和步骤进行了简要回顾。该工作的产品包括用于对与航天器工程系统相关的毛细管界面动力学进行建模的设计工具。

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