Development of Measuring System for Thermal Deformation of Heatproof Materials by Using Laser Speckle Interferometry at High Temperature

激光散斑干涉高温耐热材料热变形测量系统的研制

基本信息

  • 批准号:
    09555303
  • 负责人:
  • 金额:
    $ 7.36万
  • 依托单位:
  • 依托单位国家:
    日本
  • 项目类别:
    Grant-in-Aid for Scientific Research (B)
  • 财政年份:
    1997
  • 资助国家:
    日本
  • 起止时间:
    1997 至 1998
  • 项目状态:
    已结题

项目摘要

When the materials will be used at a high temperature atmosphere, the properties of the material must be matched with high temperature conditions. However, it is very difficult to measure the thermal strain in structures with existing methods, because the instrument used for strain measurement is in itself influenced by temperature. Electronic speckle pattern interferometry (ESPI) is a very useful method for measuring in-plane surface displacement. Using the cw-laser and the image processing system, it is possible to measure the displacement and strain : Unlike the traditional method for strain measurement such as the strain gauge or the moire method, the ESPI method requires no special surface preparation or the attachments and can measure the in-plane displacement with no contact and in real time. In this study, we discussed the use of ESPI for the measurement of the strain or the thermal strain of the objects at high temperature. And several methods to calculate the strain value from the interference fringe pattern were also discussed. In the experiments, the specimen was loaded in parallel with a load cell which provided the loading step. The specimen was a flat plate or a plate with a 12mm-diameter hole in its center. Strain gauges were attached to the specimen both in parallel and in normal directions to the loading direction. This study provides an example of how ESPI has been used to measure the two- dimensional displacement and strain distribution in the specimen. The results measured by using the ESPI were comparable with the data which were obtained by the strain-gauge method in tensile testing.
当材料要在高温环境中使用时,材料的性能必须与高温条件相匹配。然而,由于应变测量仪器本身受温度的影响,用现有的方法测量结构的热应变是非常困难的。电子散斑干涉法(ESPI)是测量面内位移的一种非常有用的方法。利用连续激光和图像处理系统,可以测量位移和应变:与应变片或云纹法等传统应变测量方法不同,ESPI方法不需要特殊的表面处理或附件,可以非接触地实时测量面内位移。在本研究中,我们讨论了利用电子散斑干涉技术来测量物体在高温下的应变或热应变。并讨论了由干涉条纹图计算应变值的几种方法。在实验中,试件与提供加载步骤的称重元件并行加载。标本为平板或中心有12 mm直径孔的平板。应变计与试件平行和垂直于加载方向连接。这项研究提供了一个例子,说明如何使用电子散斑干涉来测量试件中的二维位移和应变分布。用电子散斑干涉法测得的结果与用应变片法测得的拉伸数据具有可比性。

项目成果

期刊论文数量(0)
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Koung-Sule,Kim: "A Study on the Thesmal Expansion Analysis of Composite Materials using ESPI" 日本航空宇宙学会、西部支部講演会(1998)講演集. 234-237 (1998)
Koung-Sule, Kim:“使用 ESPI 进行复合材料热膨胀分析的研究”日本航空航天学会西部分会会议 (1998) 会议记录 234-237 (1998)。
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    0
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  • 通讯作者:
Koung-Suk Kim: "A Study on the Thermal Expansion Analysis of Composite Materials using ESPI" 日本航空宇宙学会西部支部講演会(1998)講演集. 234-237 (1998)
Koung-Suk Kim:“使用 ESPI 进行复合材料热膨胀分析的研究”日本航空学会西部分会会议记录(1998 年)234-237(1998 年)。
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    0
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  • 通讯作者:
Koung-Suk KIM,Wan-Shik JANG,Soon-Suck JARNG,Masahiko MUROZONO,Seong-Pil YANG,Hyun-Chul JUNG,and Ki-Soo KANG: "A Study on the Thermal Expansion Analysis of Composite Materials Using ESPI" Proceedings of the JSASS Seibu Branch Annual Conference. 1998. 234-2
Koung-Suk KIM、Wan-Shik JANG、Soon-Suck JARNG、Masahiko MUROZONO、Seong-Pil YANG、Hyun-Chul JUNG 和 Ki-Soo KANG:“使用 ESPI 进行复合材料热膨胀分析的研究”论文集
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MUROZONO Masahiko其他文献

MUROZONO Masahiko的其他文献

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{{ truncateString('MUROZONO Masahiko', 18)}}的其他基金

Coupled Thermoelastic Response and Its Stability of Flexible Solar Array Subjected to Radiation Heating
辐射加热下柔性太阳能电池阵的耦合热弹性响应及其稳定性
  • 批准号:
    09651009
  • 财政年份:
    1997
  • 资助金额:
    $ 7.36万
  • 项目类别:
    Grant-in-Aid for Scientific Research (C)

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  • 批准号:
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Radiative Transfer in Low Density Carbon-based and Charred Materials Under Aerodynamic Heating Conditions
气动加热条件下低密度碳基和烧焦材料的辐射传输
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    15K14251
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    2015
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    Grant-in-Aid for Challenging Exploratory Research
High-accuracy estimation of aerodynamic heating in high enthalpy flowusing Temperature-Sensitive Paint and Inverse method
利用温敏涂料和反演法高精度估算高焓流中的气动加热
  • 批准号:
    20760545
  • 财政年份:
    2008
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Control of weakly ionized flow around a reentry vehicle and aerodynamic heating by means of electromagnetic effect
利用电磁效应控制再入飞行器周围的弱电离流和气动加热
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    15206093
  • 财政年份:
    2003
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气动离解热场湍流传热模型研究
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Significant Aerodynamic Heating Phenomenon ofAblative Heatshield at Downstream Region from Stagnation Point
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  • 批准号:
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    1999
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EFFECT OF NONEQUILIBRIUM BEHIND A STRONG SHOCK UPON RE-ENTRY AERODYNAMIC HEATING
再入气动加热强冲击背后的非平衡效应
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    05452305
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"A Study on Effects of High Temperature Chemical Reactions on Shock Induced Aerodynamic Heating of Hypersonic Vehicle"
“高温化学反应对高超声速飞行器激波气动加热影响的研究”
  • 批准号:
    05650937
  • 财政年份:
    1993
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Aerodynamic Heating In Atmospheric Entry of Space Transportation
太空运输进入大气层时的气动加热
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    63550058
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    1988
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