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首页> 外文期刊>Journal of Spacecraft and Rockets >Dynamic Fluid Interface Experiments Aboard the International Space Station: Model Benchmarking Dataset
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Dynamic Fluid Interface Experiments Aboard the International Space Station: Model Benchmarking Dataset

机译:国际空间站上的动态流体界面实验:模型基准数据集

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摘要

This paper introduces a video database reduced from the handheld capillary flow contact line experiments completed aboard the International Space Station during expeditions 9-16, August 2004-November 2007. The simple fluid interface experiments quantify the uncertain impact of the boundary condition at the contact line: the region where liquid, gas, and solid meet. This region controls many significant static and dynamic characteristics of the large length scale capillary phenomena critical to multiphase fluids management systems aboard spacecraft Differences in fluid behavior of nearly identical static interfaces to nearly identical perturbations are attributed primarily to differences in fluid physics in the vicinity of the contact line. Free and pinned contact lines, large and small contact angles, and linear and nonlinear perturbations are tested for several manually imparted perturbation types (i.e., axial, slosh, and other modes) to right circular cylinders. The video and sample digitized datasets are made publicly available for model benchmarking. As a demonstration of the utility of the database, and in parallel with the experimental effort, blind numerical predictions of the dynamic interface response to the experimentally applied input perturbations are offered as an example of current capabilities to predict such phenomena. The agreement and lack of agreement between the experiments and numerics is a guide to improve or verify current analytical methods to predict such phenomena critical to practical spacecraft fluid systems design.
机译:本文介绍了一个视频数据库,该视频数据库是从2004年8月9日至16日至2007年11月的国际空间站上完成的手持式毛细管流接触线实验简化而成的。简单的流体接口实验量化了边界条件对接触线的不确定影响:液体,气体和固体相遇的区域。该区域控制着大尺度毛细管现象的许多重要的静态和动态特性,这些现象对于航天器上的多相流体管理系统至关重要,其几乎相同的静态界面至几乎相同的扰动的流体行为差异主要归因于该流体附近的流体物理学差异。接触线。对直圆柱体的几种手动传递的扰动类型(即轴向,晃动和其他模式)进行了测试,测试自由和固定的接触线,大和小的接触角以及线性和非线性扰动。视频和样本数字化数据集可公开用于模型基准测试。作为数据库实用程序的演示,并与实验工作并行,提供了动态接口对实验施加的输入扰动的响应的盲数值预测,作为当前预测此类现象的功能的示例。实验与数值之间的一致性和不一致性是改进或验证当前分析方法的指南,以预测对实际航天器流体系统设计至关重要的此类现象。

著录项

  • 来源
    《Journal of Spacecraft and Rockets》 |2010年第4期|p.670-679|共10页
  • 作者单位

    Portland State University, Portland, Oregon 97207 Department of Mechanical Engineering, P.O. Box 751-ME.;

    rnPortland State University, Portland, Oregon 97207 Department of Mechanical Engineering, P.O. Box 751-ME. AIAA;

    rnUniversity of Bremen, 28359 Bremen, Germany Center for Applied Space Technology and Microgravity, Am Fallturm;

    rnUniversity of Bremen, 28359 Bremen, Germany Center for Applied Space Technology and Microgravity;

  • 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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