| 研究課題/領域番号 |
20K14953
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| 研究種目 |
若手研究
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| 配分区分 | 基金 |
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| 審査区分 |
小区分24010:航空宇宙工学関連
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| 研究機関 | 国立研究開発法人宇宙航空研究開発機構 |
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研究代表者 |
Andrea Sansica 国立研究開発法人宇宙航空研究開発機構, 航空技術部門, 研究開発員 (80867797)
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| 研究期間 (年度) |
2020-04-01 – 2024-03-31
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| 研究課題ステータス |
交付 (2022年度)
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| 配分額 *注記 |
3,640千円 (直接経費: 2,800千円、間接経費: 840千円)
2021年度: 1,170千円 (直接経費: 900千円、間接経費: 270千円)
2020年度: 2,470千円 (直接経費: 1,900千円、間接経費: 570千円)
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| キーワード | bio-mimetic control / shock-oscillations / instability / transonic flows / Transonic buffet control / Global stability / Machine-learning / System identification / Bio-mimetic flow control / Transonic buffet / Buffet onset prediction / Buffet control / Transonic Buffet / Control / Bio-mimetic / Global Stability / Machine Learning |
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| 研究開始時の研究の概要 |
Transonic buffet consists of shock-wave oscillations that occur on aircraft wings and cause dangerous structural vibrations. By mimicking the humpback whale wavy fins, this research investigates the effectiveness of new wing configurations to suppress buffet and enhance flight quality and safety.
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| 研究実績の概要 |
Transonic buffet is an instability characterized by periodic self-sustained shock-oscillations that occur on aircraft wings at transonic conditions for increasing angles of attack. Controlling and suppressing buffet can have a significant impact in improving the aircraft overall performance and safety. To control buffet, we here proposed wings with wavy leading- and trailing edges, in the attempt to mimic the performance enhancement capabilities of the humpback whale pectoral fins. The effects of wavy leading- and trailing-edges was first tested on periodic (infinitely wide) wings at buffet conditions and it was found that wavy leading-edges are successful in suppressing the instability, while wavy trailing-edges have little or not effect. Wavy leading-edges have therefore been applied to finite wings at buffet conditions and the effect of different characteristic parameters (i.e. waviness amplitude and wavelength, waviness spanwise starting location) has been investigated. Wavy leading-edges on finite wings seem to be less effective in suppressing buffet, but the amplitude of the shock-oscillations is anyway reduced.
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| 現在までの達成度 (区分) |
現在までの達成度 (区分)
3: やや遅れている
理由
Due to the appointment of the PI to a new internal position with management tasks, some slight delayed occurred. However, the project is expected to terminate on time by the end of FY23.
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| 今後の研究の推進方策 |
Additional simulations to test different characteristic parameters are planned to determine whether further improvements in the wavy leading-edge buffet control capabilities can be obtained.
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