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Liquid-fuel droplet vaporization and cluster behavior at supercritical conditions.

机译:在超临界条件下液体燃料液滴的汽化和团簇行为。

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摘要

A systematic investigation of supercritical droplet vaporization and droplet cluster behavior has been conducted, and the research work addresses a variety of fundamental issues related to droplet vaporization and dynamics at typical conditions of liquid-propellant rocket combustion devices. A unified treatment of real-fluid thermodynamics has been developed based on fundamental theories. Special attention was given to the thermodynamic non-ideality and transport anomaly in the transcritical regime. A modified Soave-Redlich-Kwong (SRK) equation of state was utilized to derive all the thermodynamic correlations, which were then incorporated into the numerical scheme to enhance numerical efficiency and robustness. A preconditioning scheme with the dual time-stepping integration technique was implemented to render the numerical algorithm capable of treating low Mach-number fluid flows.; A series of calculations was performed to examine the cluster behavior of liquid oxygen (LOX) droplets in both sub- and super-critical hydrogen environments. The hydrogen density plays a decisive role in determining droplet interactions through its influence on the temperature and mass fraction gradients at the LOX droplet surface. In the later stage of the vaporization process, droplet vaporization rate is dominated by the oxygen accumulation at the droplet surface.; Much effort was expended to explore LOX droplet vaporization in forced-convection environments. A dimensionless parameter We1/2/ Oh, which represents the ratio of aerodynamic and viscous forces, is found to be the major factor determining the droplet deformation under supercritical conditions. Results of droplet lifetime are well correlated as a function of the initial Reynolds number and pressure. A linear relationship is generated for droplet velocity.; The interactions with two droplets moving in tandem in supercritical convective environments have been investigated. Results indicate that droplet dynamics exhibits characteristics distinct from that of an isolated droplet. A forward bag break-up of the leading droplet was found when the two droplets are initially positioned closely with a H/R ratio (the ratio of the initial droplet spacing to droplet radius) of 4 and a pressure of 100 atm. Forward movement was observed for the trailing droplet under the same condition. Increase of pressure weakens droplet interactions.
机译:已经进行了对超临界液滴蒸发和液滴团簇行为的系统研究,并且研究工作解决了在液体推进剂火箭燃烧装置的典型条件下与液滴蒸发和动力学相关的各种基本问题。基于基本理论,已经开发出了对真实流体热力学的统一处理方法。特别关注跨临界状态下的热力学非理想性和传输异常。利用改进的Soave-Redlich-Kwong(SRK)状态方程来导出所有热力学相关性,然后将这些相关性合并到数值方案中以提高数值效率和鲁棒性。实施了一种采用双重时间步长积分技术的预处理方案,以使该数值算法能够处理低马赫数流体。进行了一系列计算,以检查液氧(LOX)液滴在亚临界和超临界氢环境中的团簇行为。氢密度通过影响LOX液滴表面的温度和质量分数梯度,在确定液滴相互作用中起决定性作用。在蒸发过程的后期,液滴的蒸发速率主要由液滴表面的氧气积累决定。在强制对流环境下,人们花费了很多精力来研究LOX液滴的汽化。发现无量纲参数 We 1/2 / Oh 代表空气动力和粘性力之比,是决定空气动力和粘性动力的主要因素。超临界条件下的液滴变形。液滴寿命的结果与初始雷诺数和压力的关系密切相关。产生液滴速度的线性关系。已经研究了在超临界对流环境中两个液滴串联运动的相互作用。结果表明,液滴动力学表现出与孤立液滴不同的特征。当两个液滴最初以4的H / R比(初始液滴间距与液滴半径之比)和100 atm的压力紧密放置时,发现前导液滴的前袋破裂。在相同条件下观察到尾随液滴的向前运动。压力的增加削弱了液滴的相互作用。

著录项

  • 作者

    Meng, Hua.;

  • 作者单位

    The Pennsylvania State University.;

  • 授予单位 The Pennsylvania State University.;
  • 学科 Engineering Mechanical.; Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2000
  • 页码 197 p.
  • 总页数 197
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;航空、航天技术的研究与探索;
  • 关键词

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