### 抄録

The three-dimensional flow structure induced by normal shock-wave/boundary- layer interaction in a transonic diffuser is investigated experimentally and computationally. The experiments are done with the wall pressure measurement and oil-flow surface visualization. In the computational work, Reynolds-averaged Navier-Stokes equations are solved numerically with the κ-ω two-equation turbulence model. The solution reproduces very well the measured streamwise pressure distribution and the vortices observed in the oil-flow visualization. The careful investigation of the calculated flow reveals that the vortices are generated at the foot of the shock wave and bended downstream. It is also found that the boundary layers have a three-dimensional shape downstream of the shock wave. These flow characteristics are explained well with the simple flow model constructed by considering the wave configuration near the diffuser corner.

元の言語 | 英語 |
---|---|

ページ（範囲） | 1002-1007 |

ページ数 | 6 |

ジャーナル | Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B |

巻 | 73 |

発行部数 | 4 |

出版物ステータス | 出版済み - 4 1 2007 |

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### All Science Journal Classification (ASJC) codes

- Condensed Matter Physics
- Mechanical Engineering

### これを引用

*Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B*,

*73*(4), 1002-1007.

**Investigation of three-dimensional normal shock-wave/boundary-layer interaction in a transonic diffuser flow.** / Ono, Daisuke; Handa, Taro; Aoki, Toshiyuki; Masuda, Mitsuharu.

研究成果: ジャーナルへの寄稿 › 記事

*Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B*, 巻. 73, 番号 4, pp. 1002-1007.

}

TY - JOUR

T1 - Investigation of three-dimensional normal shock-wave/boundary-layer interaction in a transonic diffuser flow

AU - Ono, Daisuke

AU - Handa, Taro

AU - Aoki, Toshiyuki

AU - Masuda, Mitsuharu

PY - 2007/4/1

Y1 - 2007/4/1

N2 - The three-dimensional flow structure induced by normal shock-wave/boundary- layer interaction in a transonic diffuser is investigated experimentally and computationally. The experiments are done with the wall pressure measurement and oil-flow surface visualization. In the computational work, Reynolds-averaged Navier-Stokes equations are solved numerically with the κ-ω two-equation turbulence model. The solution reproduces very well the measured streamwise pressure distribution and the vortices observed in the oil-flow visualization. The careful investigation of the calculated flow reveals that the vortices are generated at the foot of the shock wave and bended downstream. It is also found that the boundary layers have a three-dimensional shape downstream of the shock wave. These flow characteristics are explained well with the simple flow model constructed by considering the wave configuration near the diffuser corner.

AB - The three-dimensional flow structure induced by normal shock-wave/boundary- layer interaction in a transonic diffuser is investigated experimentally and computationally. The experiments are done with the wall pressure measurement and oil-flow surface visualization. In the computational work, Reynolds-averaged Navier-Stokes equations are solved numerically with the κ-ω two-equation turbulence model. The solution reproduces very well the measured streamwise pressure distribution and the vortices observed in the oil-flow visualization. The careful investigation of the calculated flow reveals that the vortices are generated at the foot of the shock wave and bended downstream. It is also found that the boundary layers have a three-dimensional shape downstream of the shock wave. These flow characteristics are explained well with the simple flow model constructed by considering the wave configuration near the diffuser corner.

UR - http://www.scopus.com/inward/record.url?scp=34547314357&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=34547314357&partnerID=8YFLogxK

M3 - Article

AN - SCOPUS:34547314357

VL - 73

SP - 1002

EP - 1007

JO - Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B

JF - Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B

SN - 0387-5016

IS - 4

ER -