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Heat Loss Analysis of Flow Boiling Experiments Onboard International Space Station with Unclear Thermal Environmental Conditions (1st Report: Subcooled Liquid Flow Conditions at Test Section Inlet)

机译:热环境条件下载国际空间站流量沸腾实验的热损失分析(第1次报告:试验截面中的液流流动条件)

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Two series of flow boiling experiments have been conducted onboard the International Space Station (ISS) as a part of the TPF (Two-Phase Flow) experiment promoted by JAXA during July 2017-March 2018, February 2019-July 2019. Microgravity data on two-phase flow and heat transfer in flow boiling of n-Perfluorohexane (FC-72) have been obtained by a copper heated test tube and a transparent glass heated tube in a wide experimental range of mass velocity, liquid subcooling, vapor quality and heat flux. Furthermore, detailed two-phase flow behaviors have been observed by using high frame rate camera in the unheated observation section. In order to elucidate the accurate influence of gravity on flow boiling, it is essential to compare the heat transfer data and two-phase flow behaviors obtained under normal (terrestrial) gravity and microgravity environments at the same flow and heating conditions. However, both experiments cannot be performed by using the same experimental apparatus and under the same thermal environmental conditions. In addition, the heat loss cannot be negligible due to the forced avionics air flow inside the experimental apparatus in ISS. Therefore, exact evaluation of the fluid conditions at the inlet of the heated test tube requires the heat loss model with high-accuracy. In the present paper, the heat loss models for evaluating the degree of liquid subcooling at the inlet of the heated test tube and net heat flux from the heated tube to test fluid has been developed by using the results of preliminary heat loss experiments conducted onboard ISS. The correction of the degree of liquid subcooling by the proposed heat loss models is not negligible for the accurate analysis of gravity effects. The accuracy of the heat loss models has been verified through the evaluation of heat transfer coefficients for single-phase turbulent forced convection obtained from the heating experiments onboard ISS.
机译:在2017年7月至2019年3月2018年3月至2019年2月 - 2019年2月,国际空间站(ISS)作为TPF(两相流量)实验的一部分是TPF(两相流量)实验的一部分进行的国际空间站(ISS)的一部分进行了两系列的流沸实验。微争神通过铜加热的试管和透明玻璃加热管在质量速度,液体过冷,蒸气质量和热通量范围内获得的流沸腾中的流沸腾中的流动和热传递。 。此外,通过在未加热的观察部分中使用高帧速率相机,已经观察到详细的两相流行。为了阐明重力对流沸腾的准确影响,必须在相同的流动和加热条件下比较正常(地面)重力和微匍匐环境下获得的传热数据和两相流动。然而,两种实验不能通过使用相同的实验装置和在相同的热环境条件下进行。此外,由于ISS中的实验装置内部的强制航空电子流量,热量损失不能忽略不计。因此,加热试管入口处的流体条件的精确评估需要具有高精度的热损失模型。在本文中,通过使用初步热损失实验的结果,开发了用于评估加热试管入口处的液体过冷却度的热损失模型和从加热管对测试流体的净热通量进行开发。通过所提出的热量损失模型的液体过冷度的校正对于准确分析重力效应并不可忽略不可规定。通过评估来自在ISS的加热实验获得的单相湍流强制对流的传热系数的传热系数进行了验证了热损失模型的准确性。

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