A Study on Control of Supersonic Combustion using Mixing Enhancement by Instability Excitation
| Project/Area Number |
11450082
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| Research Category |
Grant-in-Aid for Scientific Research (B)
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| Allocation Type | Single-year Grants |
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| Section | 一般 |
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| Research Field |
Thermal engineering
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| Research Institution | The University of Tokyo |
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Principal Investigator |
KONO Michikata Graduated School of Frontier Sciences, University of Tokyo, Professor, 大学院・新領域創成化学研究科, 教授 (60011194)
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| Co-Investigator(Kenkyū-buntansha) |
UJIIE Yasushige Faculty of Industrial Engineering, Nihon University, Professor, 生産工学部, 教授 (20060197)
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| Project Period (FY) |
1999 – 2001
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| Project Status |
Completed (Fiscal Year 2001)
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| Budget Amount *help |
¥15,000,000 (Direct Cost: ¥15,000,000)
Fiscal Year 2001: ¥1,300,000 (Direct Cost: ¥1,300,000)
Fiscal Year 2000: ¥2,800,000 (Direct Cost: ¥2,800,000)
Fiscal Year 1999: ¥10,900,000 (Direct Cost: ¥10,900,000)
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| Keywords | Supersonic Flow / Instability / Mixing Enhancement / Combustion Enhancement / Supersonic Combustion Ram Jet Engine / 圧縮性流れ / スクラムジェット・エンジン / 超音速燃焼 / 乱流混合 / 音波擾乱 / 燃焼制御 / 圧縮性流体 / 音波じょう乱 / 燃焼効率 |
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| Research Abstract |
The objective of the present study is to investigate experimentally mixing enhancement of fuel and air and combustion enhancement in supersonic air flows. The instability of the mixing layer which formed between air flow and fuel flow is excited by injection of the acoustic disturbances. The cavity which is located on the wall of the flow channel is used as the source of acoustic disturbances. The mixing enhancement is expected to be appeared by acoustic disturbances, and consequently the combustion efficiency is expected to increase.
Non-Combustion Experiments : Experiments without combustion are conducted at the first stage in order to investigate effects of acoustic disturbance on the growth of the mixing layer. Hydrogen is injected as a gaseous fuel parallel to the supersonic air flow. The acoustic disturbance is injected to the supersonic mixing layer in order to explore mixing enhancement by acoustic disturbances. Measurements of Pilot pressure distribution in the mixing layer is
… More
conducted and Schlieren photography is used for the visualization of the mixing layer by a CCD camera with the image intensifies The results show that the growth rate of the mixing layer is larger with the acoustic disturbance than that without it. This suggests that the injection of the acoustic disturbance is effective for the enhancement of the mixing of air and fuel.
Combustion Experiments : The acoustic disturbance is injected to the mixing layer with combustion and the combustion efficiency is obtained in order to investigate effects of mixing enhancement mentioned above on the combustion behavior. The combustion efficiency is obtained from the measured wall pressure profiles in the combustion chamber. The combustion efficiency with the acoustic disturbance is larger than that without it. The results also show that the intense combustion mode appears stably using acoustic disturbances.
These results indicate that, the injection of the acoustic disturbance is useful for the enhancement of mixing and increase in the combustion efficiency in the supersonic flow. Less
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Report
(4 results)
Research Products
(11 results)
