Measurement of Supersonic Injection Flowfield Using Acetone PLIF
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- Takahashi Hidemi
- 東北大学大学院工学研究科航空宇宙工学専攻
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- Hirota Mitsutomo
- 東北大学大学院工学研究科航空宇宙工学専攻
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- Oso Hiroki
- 東北大学大学院工学研究科航空宇宙工学専攻
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- Masuya Goro
- 東北大学大学院工学研究科航空宇宙工学専攻
Bibliographic Information
- Other Title
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- 超音速噴射流れ場におけるアセトンPLIF計測
- チョウオンソク フンシャ ナガレバ ニ オケル アセトン PLIF ケイソク
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Abstract
Structure of flow field formed by normal sonic injection into a Mach 1.8 air stream was investigated with acetone planar laser induced fluorescence (acetone PLIF). Parametric calculation of fluorescence intensity indicates that it represent molar concentration within ±2.5% error for the present experimental condition. For the special situation of isentropic flow without any mixing, Mach number can be deduced from the fluorescence intensity. Mach number distribution from PLIF data was compared with one obtained from PIV measurement, and showed good agreement. The jet trajectories obtained from images visualized by acetone PLIF and Mie scattering are compared. We find that the acetone PLIF gives reasonable trajectory while the Mie scattering over estimate the jet penetration.
Journal
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- JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 55 (642), 318-323, 2007
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Keywords
Details 詳細情報について
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- CRID
- 1390282679447456000
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- NII Article ID
- 10019783880
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- NII Book ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL BIB ID
- 8893887
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed