Numerical Simulation and Experiment of Supersonic Jet Impingement on a Plate.
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- TSUBOI Nobuyuki
- 東京大学大学院工学系研究科機械工学専攻
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- HAYASHI A. Koichi
- 青山学院大学理工学部機械工学科
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- FUJIWARA Toshitaka
- 名古屋大学工学研究科
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- ARASHI Kazuo
- 熊本工業大学工学部構造工学科
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- KODAMA Masaru
- 三菱重工業 (株) 名古屋航空宇宙システム製作所
Bibliographic Information
- Other Title
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- 平板に衝突する超音速噴流に関する数値解析及び実験
- ヘイバン ニ ショウトツ スル チョウオンソク フンリュウ ニ カンスル スウ
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Abstract
An impingement of two-dimensional axisymmetric supersonic jet on a plate is simulated numerically to evaluate the jet flow configuration on the plate with a real gas assumption. An explicit TVD-Upwind scheme is used for the Euler equations to evaluate interaction between shock waves. An experimental study of the underexpanded axisymmetric supersonic N2 jets impinging on a plate is also discussed. Pressure measurements on the plate surface and Schlieren photometries are performed to investigate the impinging jets. Numerical results with the Euler equations have a good agreement with the experimental results at the shock structure and pressure distribution on the plate. The results show that three types for complicated shock-shock interactions are revealed and that a stagnation bubble is formed due to triple point near the plate.
Journal
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- Aeronautical and Space Sciences Japan
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Aeronautical and Space Sciences Japan 46 (536), 485-496, 1998
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390282679454737920
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- NII Article ID
- 10002863045
- 10006924422
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- NII Book ID
- AN00189072
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- ISSN
- 24241369
- 00214663
- http://id.crossref.org/issn/13446460
- http://id.crossref.org/issn/00214663
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- NDL BIB ID
- 4553825
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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