1.0%の微細粗さで空気抵抗43.6%低減を世界で初実証 ―流体工学80年の常識を覆す発見、航空機などの省エネに期待―

2026-05-12 東北大学

東北大学流体科学研究所の研究グループは、流線型物体表面にミクロンサイズの不規則な微細粗さ「DMR(Distributed Micro-Roughness)」を施すことで、空気抵抗を最大43.6%低減できることを世界で初めて実証した。従来は「表面は滑らかなほど抵抗が小さい」と考えられてきたが、本研究はその80年来の常識を覆す成果となる。研究では、38~53μmの微細凹凸を形成した模型を、東北大学の世界最大級「1m磁力支持天秤装置(MSBS)」で非接触浮揚させ、支持棒による気流乱れを排除した高精度風洞実験を実施した。さらに数値流体解析やオイルフロー可視化により、抵抗低減の主因が剥離抑制ではなく、層流維持による壁面摩擦抵抗そのものの低減であることを定量的に証明した。微細粗さが乱流遷移を遅延させることで抵抗低減が生じると考えられ、航空機、自動車、ドローンなど輸送機器の省エネルギー化への応用が期待される。

1.0%の微細粗さで空気抵抗43.6%低減を世界で初実証 ―流体工学80年の常識を覆す発見、航空機などの省エネに期待―
図1. 東北大学流体科学研究所の1m磁力支持天秤装置(1m-MSBS)で浮揚された流線型模型

<関連情報>

磁気浮上式バランスシステムで測定した、流線型物体の抗力低減に対するDMR効果 DMR effect on drag reduction of a streamlined body measured by magnetic suspension and balance system

Aiko Yakeno[,Hiroyuki Okuizumi,Kento Inokuma and Yoshiyuki Watanabe
Journal of Fluid Mechanics  Published:07 May 2026
DOI:https://doi.org/10.1017/jfm.2026.11520

Abstract

This study experimentally investigates the aerodynamic drag reduction capabilities of distributed micro-roughness (DMR) coatings on a streamlined model, utilising the 1-m magnetic suspension and balance system (MSBS) at Tohoku University. Previous direct numerical simulations indicated that DMR can mitigate turbulent-energy growth by suppressing Tollmien–Schlichting waves and influencing the breakdown of streamwise vortices. The present work provides the first experimental validation of these effects using an interference-free MSBS, which is essential for accurate measurement in the laminar and transitional regimes. A streamlined model was tested with two rows of artificial tripping tape to induce transition; the DMR height was approximately 1 % of the local boundary layer thickness, significantly smaller than typical roughness elements. Direct aerodynamic drag measurements using the MSBS revealed a substantial reduction of up to 43.6 % within the transitional flow regime. Crucially, integrated analysis using wall-resolved large eddy simulations (LES) and dynamic oil-flow visualisation confirmed that this benefit does not mainly originate from the suppression of flow separation. The LES drag decomposition established that the total pressure-drag budget is subordinate to skin friction, a finding complemented by oil-flow observations, which revealed qualitatively similar flow patterns regardless of the surface condition. Consequently, the observed drag reduction is primarily ascribed to friction drag reduction achieved through the modification of the boundary layer state. These findings provide compelling experimental evidence for the efficacy of DMR and offer valuable insights for optimising surface designs for passive flow control.

0106流体工学
ad
ad
Follow
ad
タイトルとURLをコピーしました