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首页> 外文期刊>Journal of combustion >Combustion of Submillimeter Heptane/Methanol and Heptane/Ethanol Droplets in Reduced Gravity
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Combustion of Submillimeter Heptane/Methanol and Heptane/Ethanol Droplets in Reduced Gravity

机译:在重力降低的情况下燃烧亚毫米庚烷/甲醇和庚烷/乙醇液滴

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摘要

Reduced-gravity experiments were performed on combustion of droplets composed of n-heptane mixed with methanol or ethanol. The initial alcohol mass fraction in a droplet was 0% (pure heptane) or 5%. The experiments were performed at 0.1 MPa and 25℃ with air or with ambients of oxygen and helium with oxygen mole fractions of 0.3 or 0.4. Initial droplet diameters were in the range 0.67 mm to 0.92 mm. After considering measurement uncertainties, burning rates decreased appreciably as the initial droplet diameter increased for combustion in air but not for combustion in the oxygen/helium environments. It was also found that addition of either methanol or ethanol did not influence burning rates appreciably and that burning rates were larger for the oxygen/helium environments than for air if initial droplet diameter dependences were accounted for.
机译:对由正庚烷与甲醇或乙醇混合组成的液滴燃烧进行了重力降低实验。液滴中的初始醇质量分数为0%(纯庚烷)或5%。实验是在0.1 MPa和25℃,空气或氧气和氦气的环境下进行的,氧气的摩尔分数为0.3或0.4。初始液滴直径在0.67mm至0.92mm的范围内。在考虑了测量的不确定性之后,燃烧速率随着初始液滴直径的增加而明显降低,这是在空气中燃烧所产生的,而在氧气/氦气环境中则没有发生。还发现添加甲醇或乙醇均不会明显影响燃烧速率,并且如果考虑到初始液滴直径的依赖性,氧气/氦气环境的燃烧速率比空气的燃烧速率大。

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  • 来源
    《Journal of combustion》 |2013年第2013期|154202.1-154202.6|共6页
  • 作者

    I. Aharon; V. K. Tam; B. D. Shaw;

  • 作者单位

    Mechanical and Aerospace Engineering Department, University of California, Davis, CA 95616, USA Rafael Haifa 31021, Israel;

    Mechanical and Aerospace Engineering Department, University of California, Davis, CA 95616, USA Tesla Motors, 3500 Deer Creek Road, Palo Alto, CA 94304, USA;

    Mechanical and Aerospace Engineering Department, University of California, Davis, CA 95616, USA;

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