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Basic study for developing supercritical spray combustion simulator

Basic study for developing supercritical spray combustion simulator
超临界喷雾燃烧模拟器研制基础研究
批准号:
04650173
负责人:
UMEMURA Akira
金额:
$1.28万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for General Scientific Research (C)
财政年份:
1992
资助国家:
日本
项目状态:
已结题
起止时间:
1992 至 1993

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中文摘要
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英文摘要
Numerical simulations were performed to examine the vaporization/cobustion characteristics for a liquid fuel droplet which was suddenly placed in an otherwise quiescent, inert/oxidizing gas at various status beyond the critical point of the fues. The vaporization/combustion characteristics were fully disclosed, together with their underlying physics. For a given ambient gas temperature, the minimum gasification/combustion time is achieved at such a pressure that the surface temperature which the droplet assumes immediately after its exposure to the hot inert gas or ignition coincides with the 'mixture' critical temperature. This pressure is far above the fuel critical pressure for a droplet gasifying in the ambient gas at a relatively low temperature, whereas the presence of flame shifts it very cose to the fuel critical pressure. Three modes of droplet vaporization were identified in the parameter space of ambient gas temperature and pressure ; (1) In the subcritical vaporization regi … More me, the droplet has the surface throughout its lifetime. (2) In the supercritical gasification regime, spatially continuous phase change occurs from the beginning. (3) Between them, there is the transient vaporization regime in which the transition from the sub-to-supercritical vaporization mode takes place.A generalized asymptotic theory was constructed to gain insight into the interactive droplet vaporization and combustion property in spray. At high pressures, a spray can be regarded as an ensemble of independent droplets pressures because the range of influence of each droplet is restricted within a short distance. A new numerical calculation method which incorporates the inherently unsteady droplet vaporization and combustion property was developed in order to transform a low-pressure spray combustion simulator at hand to a high-pressure one, in which the movements of a great number of droplets can be pursued in a Lagrangian way. Dynamic phenomena which would appear when the surface tension of droplet diminishes or vanishes were examined to approach the masked dynamic behaviors of sprays in supercritical conditions. Less
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通讯作者:
梅村,可知: "だ円渦モデルによる大規模渦構造の記述" 機論(B編). 59. 319-325 (1993)
Umemura, Kachi:“使用椭圆涡模型描述大尺度涡结构”机制(B 版)。
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23
    Development of a new conceptual atomization simulator for liquid rocket engines
    Development of a genuine numerical simulator for spray combustion based on new concepts derived from microgravity experiments
    • 批准号:
      18360404
    • 项目类别:
      Grant-in-Aid for Scientific Research (B)
    • 资助金额:
      $9.2万
    • 财政年份:
      2006
    • 负责人:
      UMEMURA Akira
    • 依托单位:
    Study on the instability of near-critical-mixing surface jet and turbulent atomization for the purpose of high-pressure spray combustion control
    • 批准号:
      14350510
    • 项目类别:
      Grant-in-Aid for Scientific Research (B)
    • 资助金额:
      $8.51万
    • 财政年份:
      2002
    • 负责人:
      UMEMURA Akira
    • 依托单位:
    Study on the Atomization Gasification, Mixing and Combustuin Processes of Liquid fuel Jets in Supercritical Enironments
    • 批准号:
      11650219
    • 项目类别:
      Grant-in-Aid for Scientific Research (C)
    • 资助金额:
      $1.66万
    • 财政年份:
      1999
    • 负责人:
      UMEMURA Akira
    • 依托单位:
    海外基金