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Surface temperature of agglomerated aluminum particles in a reaction zone

机译:反应区团聚铝颗粒的表面温度

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摘要

Aluminum particles are used as a metal fuel to increase the propulsion performance of composite propellants in solid rockets. As such, the combustion mechanism of aluminum has received considerable research attention. Aluminum gas reacts with surrounding oxidizers and creates the diffusion flame. The evaporation time is proportional to the square of the particle diameter, with a constant of proportionality that depends on the temperature difference between the luminous flame and the agglomerated aluminum particle surface. The luminous flame temperature is easily obtained theoretically, but the surface temperature is yet to be obtained experimentally. If the surface temperature could be obtained, the difference between the boiling temperature and the surface temperature of aluminum particles would be clarified. Therefore, it is necessary to study the agglomerated aluminum particle surface. In this study, the dependence of aluminum particle surface on the atmospheric pressure and on the particle diameter is investigated. It is established that the surface temperature is lower than the boiling temperature of aluminum. The mean surface temperature is a constant with respect to the particle diameter from 100 to 500 μm at 0.1 MPa. Also, it is clarified that the surface temperature is determined by energy balance at aluminum particle surface.
机译:铝颗粒用作金属燃料,以提高固体火箭中复合推进剂的推进性能。因此,铝的燃烧机理已受到相当多的研究关注。铝与周围的氧化剂发生反应并产生扩散火焰。蒸发时间与颗粒直径的平方成正比,比例常数取决于发光火焰与团聚的铝颗粒表面之间的温差。发光火焰温度在理论上很容易获得,但表面温度尚未通过实验获得。如果能够获得表面温度,则将澄清沸腾温度与铝颗粒的表面温度之间的差异。因此,有必要研究附聚的铝颗粒表面。在这项研究中,研究了铝颗粒表面对大气压和颗粒直径的依赖性。已经确定表面温度低于铝的沸腾温度。在0.1MPa下,平均表面温度相对于100至500μm的粒径是恒定的。另外,明确了表面温度由铝粒子表面的能量平衡决定。

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  • 来源
    《Journal of propulsion and power》 |2017年第6期|1351-1357|共7页
  • 作者单位

    Nihon University, Chiba, Japan,Department of Aerospace Engineering, College of Science and Technology, 7-24-1, Narashino-dai, Funabashi, Japan;

    Nihon University, Chiba, Japan,Department of Aerospace Engineering, College of Science and Technology, 7-24-1, Narashino-dai, Funabashi, Japan;

    IHI Aerospace, Gunma, Japan,Development Office, Technologies Development Department, 900 Fujiki, Tomioka, Japan;

    IHI Aerospace, Gunma, Japan,Development Office, Technologies Development Department, 900 Fujiki, Tomioka, Japan;

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