DEVELOPMENTAL SCIENTIFIC RESEARCH ON CERAMIC CONTROLLABLE-STRUT FOR SUPERSONIC COMBUSTION
DEVELOPMENTAL SCIENTIFIC RESEARCH ON CERAMIC CONTROLLABLE-STRUT FOR SUPERSONIC COMBUSTION
批准号:
05555258
负责人:
NIIOKA Takashi
金额:
$4.16万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Developmental Scientific Research (B)
财政年份:
1993
资助国家:
日本
项目状态:
已结题
起止时间:
1993 至 1994
中文摘要
针对冲压发动机和超燃冲压发动机提出了一种在试验台上制作的支撑板,并在马赫数为1.5的超音速气流中进行了燃烧试验。该支柱模型由两部分组成,按流向划分,一部分支柱可以改变,例如,根据气流状况。因此,预计在任何燃料和空气条件下都可以进行阻燃。这种可控支柱的两个部分之间的间隙可以改变到60 mm,而且后支柱的移动速度也可以改变。结果表明,阻燃性能有所改善,但由于流动的不稳定性,其阻燃性能依赖于移动速度。支柱是陶瓷制成的,可加工性很好,即使经过多次十秒的实验也没有问题。
英文摘要
A newly devised strut made on an experimental bais was proposed for the ramjet or scramjet engine and its combustion experiments were carried out in supersonic airflow of Mach number 1.5. This strut model is composed of two parts divided streamwise and a part of the strut can be changed, for example, in response to airflow condition. Therefore, it is expected that the flame-holdindg is always possible in any condition of fuel and air. The intervening space between two parts of this controllable strut can be changed up to 60 mm and also the moving speed of the rear strut can be variable. It was found that the flame-holding characteristics were improved, but that they depended on the moving speed beacause of its unstesdiness of the flow. The strut was made of ceramics, whose machinability was so good, and had no problem even after many times of ten-second experiment.
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M.Uchiumi,H.Kobayashi,S.Hasegawa,T.Niioka: "Flame-Holding Mechanism of a Newly Devised Strut for Scramjet Engine" Transactions of the Japan Society for Aeronautical and Space Sciences. (in press) (1995)
M.Uchiumi、H.Kobayashi、S.Hasekawa、T.Niioka:“超燃冲压发动机新设计支柱的火焰保持机构”日本航空航天学会会刊。
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通讯作者:
M.Uchiumi, H.Kobayashi, S.Hasegawa and T.Niioka: "Flame-Holding Mechanism of a Newly Devised Strut for Scramjet Engine" Transactions of the Japan Society for Aeronautical and Space Sci.in press.
M.Uchiumi、H.Kobayashi、S.Hasekawa 和 T.Niioka:“新设计的超燃冲压发动机支柱的火焰保持机构”,日本航空航天学会会刊,出版。
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T.Niioka,K.Terada,H.Kobayashi and S.Hasegawa: "Flame Stabilization Characteristics of Strut Divided into Two Parts in Supersonic Airflow" Journal of Propulsion and Power. 11. 112-116 (1995)
T.Niioka、K.Terada、H.Kobayashi 和 S.Hasekawa:“超音速气流中分为两部分的支柱的火焰稳定特性”推进与动力杂志。
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T.Niioka,K.Terada,H.Kobayashi and S.Hasegawa: "Flame Stabilization Characteristics of Strut Divided into Two Parts in Supersonic Airflow" Propulsion and Power,AIAA. (発表予定). (1994)
T. Niioka、K. Terada、H. Kobayashi 和 S. Hasekawa:“超音速气流中支柱的火焰稳定特性”推进与动力,AIAA(即将发表)。
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Y.Ju and T.Niioka: "Structure and Extinction of a Diffusion Flame with Chain Mechanism in Supersonic Mixing Layer" Transactions of the Japan Society for Aeronautical and Space Sciences. 37. 148-163 (1994)
Y.Ju 和 T.Niioka:“超音速混合层中链式扩散火焰的结构和熄灭”日本航空航天学会会刊。
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共 16 条
Study of the Effect of Shock Wave on Fuel Injection and Combustion
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批准号:14350505
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项目类别:Grant-in-Aid for Scientific Research (B)
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资助金额:$9.15万
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财政年份:2002
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负责人:NIIOKA Takashi
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依托单位:
Research and Development of Two-staged Combustion Strut with Air Intake
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批准号:10555332
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项目类别:Grant-in-Aid for Scientific Research (B)
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资助金额:$1.92万
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财政年份:1998
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负责人:NIIOKA Takashi
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依托单位:
CLALIFICATION OF FUNDAMENTAL PHENOMENA ON NON-EMISSION BURNING OF CO_2AND NOx
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批准号:10450078
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项目类别:Grant-in-Aid for Scientific Research (B).
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资助金额:$5.31万
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财政年份:1998
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负责人:NIIOKA Takashi
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依托单位:
Research and Development of Supersonic Combustion Strut with a Preburner
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批准号:07555678
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项目类别:Grant-in-Aid for Scientific Research (A)
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资助金额:$2.11万
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财政年份:1995
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负责人:NIIOKA Takashi
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依托单位:
Evaporation and Ignition of Liquid Fuels at Critical Pressure Regime.
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批准号:06452180
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项目类别:Grant-in-Aid for Scientific Research (B)
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资助金额:$2.56万
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财政年份:1994
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负责人:NIIOKA Takashi
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依托单位:
海外基金