### 抜粋

A series of large-eddy simulations of spatially developing turbulent boundary layers with uniform blowing at moderate Reynolds numbers (based on free-stream velocity, U_{∞} and momentum thickness, θ) up to Reθ ∼ 2500 were performed with the special focus on the effect of intermittent (separated in streamwise direction) blowing sections. The number of blowing sections, N, investigated is set to be 3, 6, 20, 30 and compared to N = 1, which constitutes the reference case, while the total wall-mass flux is constrained to be the same for all considered cases, corresponding to a blowing amplitude of 0.1% of U_{∞} for the reference case. Results indicate that the reference case provides a net-energy saving rate of around 18%, which initially decreases at most 2 percentage points for N = 3 but recovers with increasing N. The initial reduction of the drag reduction is due to the shorter streamwise length of intermittent blowing sections. The physical decomposition of the skin friction drag through the FIK identity (Fukagata et at, 2002), shows that the distribution of all components over each blowing section has similar trends, resulting in similar averaged values over the whole control region.

元の言語 | English |
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ホスト出版物のタイトル | 9th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2015 |

出版者 | TSFP-9 |

巻 | 1 |

ISBN（電子版） | 9780000000002 |

出版物ステータス | Published - 2015 1 1 |

イベント | 9th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2015 - Melbourne, Australia 継続期間: 2015 6 30 → 2015 7 3 |

### Other

Other | 9th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2015 |
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国 | Australia |

市 | Melbourne |

期間 | 15/6/30 → 15/7/3 |

### ASJC Scopus subject areas

- Fluid Flow and Transfer Processes

## フィンガープリント Drag reduction in spatially developing turbulent boundary layers by blowing at constant mass-flux' の研究トピックを掘り下げます。これらはともに一意のフィンガープリントを構成します。

## これを引用

*9th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2015*(巻 1). TSFP-9.