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首页> 外文期刊>Journal of Thermophysics and Heat Transfer >Measurement of Heat Transfer Rate on Backward-Facing Steps at Hypersonic Mach Number
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Measurement of Heat Transfer Rate on Backward-Facing Steps at Hypersonic Mach Number

机译:高超声速马赫数下向后步骤传热速率的测量

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摘要

Two backward-facing models with step heights of 2 and 3 mm are used to measure the convective surface heatntransfer rates by using platinum thin-film gauges, deposited on Macor inserts. Heat transfer rates have beenntheoretically calculated along the flat plate portion of a model using the Eckert reference temperature method. Thenexperimentally determined surface heat transfer rate distributions are compared with theoretical and numericalnestimations. Experimental heat flux distribution over a flat plate model showed good agreement with the referencentemperature method at stagnation enthalpy range of 0:8–2 = . Theoretical analysis has been used forndownstream of a backward-facing step using Gai’s nondimensional analysis. It has been found from the presentnstudy that approximately 10 and 8 step heights are required for the flow to reattach for 2 and 3 mm step heightnbackward-facing step models, respectively, at a nominal Mach number of 7.6.
机译:两个台阶高度分别为2和3 mm的朝后模型用于通过沉积在Macor刀片上的铂金薄膜量规来测量对流表面传热速率。理论上,已经使用埃克特参考温度方法沿模型的平板部分计算了传热速率。然后将实验确定的表面传热速率分布与理论和数值模拟进行比较。在平板焓模型上,当滞热焓为0:8–2 =时,实验热通量分布与参考温度方法显示出良好的一致性。理论分析已用于通过盖氏的无量纲分析进行的向后步骤的下游。从目前的研究中发现,对于标称马赫数为7.6的向后台阶模型,分别需要2到3 mm台阶高度的流动,需要大约10和8台阶高度。

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  • 来源
    《Journal of Thermophysics and Heat Transfer》 |2011年第3期|p.321-328|共8页
  • 作者单位

    P. Reddeppa∗Airbus Engineering Centre India Pvt. Ltd., Bangalore 560 016, IndiaK. Nagashetty,†S. Saravanan,‡and G. Jagadeesh§Indian Institute of Science, Bangalore 560 012, IndiaandS. L. Gai¶University of New South Wales, Canberra ACT 2600, Australia;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
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  • 正文语种 eng
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