Updated on 2025/04/22

Information

 

写真a

 
Yuichi Kuya
 
Organization
Faculty of Engineering Department of Aeronautics and Astronautics Associate Professor
Faculty of Engineering Department of Aeronautics and Astronautics(Concurrent)
Title
Associate Professor
Contact information
メールアドレス

Research Areas

  • Informatics / Computational science

  • Frontier Technology (Aerospace Engineering, Marine and Maritime Engineering) / Aerospace engineering

  • Manufacturing Technology (Mechanical Engineering, Electrical and Electronic Engineering, Chemical Engineering) / Fluid engineering

Degree

  • PhD

Research History

  • Kyushu University Department of Aeronautics and Astronautics Associate Professor 

    2025.1 - Present

  • Tohoku University Graduate School of Engineering Department of Aerospace Engineering Associate Professor 

    2022.4 - 2024.12

  • Tohoku University Graduate School of Engineering Assistant Professor 

    2016.10 - 2022.3

  • Mercedes-AMG Petronas Formula One Team  CFD aerodynamicist 

    2012.1 - 2016.9

  • University of Southampton  Research fellow 

    2011.5 - 2011.12

Awards

  • 日本流体力学会賞 (論文賞)

    2022.12   日本流体力学会  

    久谷雄一, 戸谷晃輔, 河合宗司

  • 第51回流体力学講演会/第37回航空宇宙数値シミュレーション技術シンポジウム 最優秀賞 (航空宇宙数値シミュレーション技術部門)

    2019.9   日本航空宇宙学会 / 国立研究開発法人 宇宙航空研究開発機構  

    久谷雄一, 河合宗司

Papers

  • Secondary conservation properties of compact schemes in split forms Reviewed

    Y. Kato, Y. Kuya

    Journal of Computational Physics   528   113829-1 - 113829-18   2025.5   ISSN:0021-9991 eISSN:1090-2716

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    Authorship:Corresponding author   Publisher:Journal of Computational Physics  

    This study theoretically proves that the properties of kinetic energy preservation and product rule discretely hold in a non-dissipative numerical scheme based on a compact scheme. A previous work developed a kinetic energy and entropy preserving (KEEP) compact scheme and showed superior numerical stability compared to the standard compact scheme. However, the reason for the improved numerical stability in the KEEP-compact scheme was not clearly discussed in the previous work. This study reviews the construction of the compact scheme using the Padé approximation and shows that the important discrete properties of kinetic energy preservation and product rule, which play major roles in improving numerical stability in the existing explicit KEEP schemes, hold in the KEEP-compact scheme.

    DOI: 10.1016/j.jcp.2025.113829

    Web of Science

    Scopus

  • Similarities between directed percolation and boundary layer transition on a flat plate Reviewed

    Y. Kuya, H. Murakami, T. Ariki, K. Sawada

    Journal of the Physical Society of Japan   93 ( 11 )   114003-1 - 114003-7   2024.11   ISSN:0031-9015 eISSN:1347-4073

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    Authorship:Lead author, Corresponding author   Publishing type:Research paper (scientific journal)   Publisher:Physical Society of Japan  

    This study examines the similarity between directed percolation (DP) and boundary layer transition on a flat plate, performing large eddy simulation (LES).A flat-plate boundary-layer flow is one of the well-studied fundamental flows and is widely used in developing turbulence and transition models.In this study, laminar-turbulent transition is enforced on a flat plate by a blowing-suction wall-normal velocity given at the upper computational boundary.Since the separated shear layer plays a major role in causing laminar-turbulent transition in the flow field studied in this study, the relation between the transition and DP is investigated on a constant plane along the separated shear layer.The DP universality class is characterized by some critical exponents, and two of the three critical exponents obtained by the present LES are in good agreement with the one-dimensional DP universality class.

    DOI: 10.7566/JPSJ.93.114003

    Web of Science

    Scopus

  • Quantum annealing-based algorithm for lattice gas automata Reviewed

    Y. Kuya, K. Komatsu, K. Yonaga, H. Kobayashi

    Computers & Fluids   274   106238-1 - 106238-7   2024.4   ISSN:0045-7930 eISSN:1879-0747

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    Authorship:Lead author, Corresponding author   Publishing type:Research paper (scientific journal)   Publisher:Computers and Fluids  

    This study proposes a quantum annealing-based algorithm for flow computation based on lattice-gas automata (LGA). Since the state of the lattice gas is determined by Boolean variables, 0 (absence) or 1 (presence), in LGA, it is well suited for implementation in quantum annealing and simulated annealing computers. The quantum annealing-based algorithm proposed in this study is constructed so that conservation of mass and momentum is satisfied at the particle collision process. Verification tests performed with various quantum annealing and simulated annealing computers confirm that the proposed algorithm well replicates a conventional LGA collision model.

    DOI: 10.1016/j.compfluid.2024.106238

    Web of Science

    Scopus

  • A kinetic energy and entropy preserving (KEEP) finite volume scheme on unstructured meshes for compressible flows Reviewed

    Yuichi Kuya, Wataru Okumura, Keisuke Sawada

    Journal of Computational Physics   491   112521-1 - 112521-22   2023.12   ISSN:0021-9991 eISSN:1090-2716

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    Authorship:Lead author, Corresponding author   Publishing type:Research paper (scientific journal)   Publisher:Journal of Computational Physics  

    A kinetic energy and entropy preserving (KEEP) finite-volume scheme on unstructured meshes is proposed for non-dissipative and stable compressible flow computations. The KEEP finite volume scheme proposed in the present study is based on the existing KEEP schemes developed for finite difference methods. The KEEP schemes have shown superior numerical robustness without numerical dissipation in previous studies. The KEEP schemes are discretized such that the numerical fluxes discretely replicate the key analytical relations that the governing equations hold, leading to preservation of kinetic energy and a superior entropy preservation property in the incompressible and inviscid limits. This study proposes using cell-vertex discretization for the proposed KEEP finite volume scheme in order to maintain this characteristic property of the KEEP scheme and achieve second-order accuracy in space on simplex meshes and arbitrary meshes that are not highly irregular. In the numerical tests performed in this study, the proposed KEEP finite volume scheme successfully performs long-time stable computations on various unstructured meshes. Also, the proposed KEEP scheme shows much better numerical stability and spatial accuracy than the KEEP scheme with cell-centered discretization.

    DOI: 10.1016/j.jcp.2023.112521

    Web of Science

    Scopus

  • A DES study of the flow around a full-scale train under crosswind condition Reviewed

    T. Ariki, Y. Shibasaki, Y. Kuya, M. Adachi, K. Sawada

    Mechanical Engineering Letters   9 ( 0 )   22-00464-1 - 22-00464-99   2023.6   eISSN:21895236

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    Language:English   Publishing type:Research paper (scientific journal)   Publisher:The Japan Society of Mechanical Engineers  

    <p>A numerical study on the flow around a full-scale train subjected to crosswind has been conducted on the basis of detached-eddy simulation (DES). Finite-volume method is applied to unstructured mesh generated around a three-car-train model whose running speed is fixed to 120 km/h while the crosswind speed is set to 5 m/s,15 m/s, and 25 m/s. A clear longitudinal vortex structure is recognized in the case of the crosswind speed of 25 m/s, where two longitudinal vortices are evolved respectively from the roof and floor of the head car (roof-edge and floor-edge vortices), forming a characteristic vortex pair. This longitudinal vortex structure around the head car is discussed with a focus on its non-trivial role in the side-force mechanism. Our simulation suggests a causal association between these two vortices, which implies an importance of optimum designing of the underfloor equipment in addition to the roof and head shapes of the head car.</p>

    DOI: 10.1299/mel.22-00464

    CiNii Research

  • Blending of Reynolds Stress Transport Model and γ Transition Model Reviewed

    Yuichi Kuya, Taketo Ariki, Shunya Endo, Thanakorn Sujisakulvong, Keisuke Sawada

    AIAA Journal   61 ( 2 )   940 - 949   2023.2   ISSN:0001-1452 eISSN:1533-385X

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    Authorship:Lead author, Corresponding author   Publisher:American Institute of Aeronautics and Astronautics (AIAA)  

    DOI: 10.2514/1.J061781

    Web of Science

    Scopus

  • Comprehensive analysis of entropy conservation property of non-dissipative schemes for compressible flows: KEEP scheme redefined Reviewed

    Yoshiharu Tamaki, Yuichi Kuya, Soshi Kawai

    Journal of Computational Physics   468   111494-1 - 111494-22   2022.11   ISSN:0021-9991 eISSN:1090-2716

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    Publishing type:Research paper (scientific journal)   Publisher:Elsevier BV  

    A theoretical analysis of the entropy conservation properties is conducted to explain the different behaviors of the non-dissipative finite-difference spatial discretization schemes, such as the kinetic-energy and entropy preserving (KEEP) schemes. The analysis is conducted based on the spatially-discretized entropy-evolution equation derived from the Euler equations with retaining the discrete-level strictness. The present analysis shows that the analytical relations (ARs) employed by the KEEP schemes eliminate some terms of the discretized entropy-evolution equation and help simplify the equation, while the ARs are not sufficient to explain the entropy-conservation property. Therefore, the entropy error is decomposed into several terms, and the behaviors of those decomposed error terms are observed in the compressible inviscid Taylor–Green vortex test case. The results of the test case show that the terms containing the velocity difference between two grid points cause significant entropy conservation error and result in the different entropy conservation properties of the tested non-dissipative schemes. Furthermore, the KEEP schemes are redefined based on the present entropy-error analysis. In the redefined KEEP schemes, the formulation does not contain logarithmic means, and the strictness of entropy conservation can be adjusted easily by the truncation order of the Maclaurin expansions. Finally, the present entropy-error analysis and the redefined KEEP schemes are extended to the generalized curvilinear coordinates.

    DOI: 10.1016/j.jcp.2022.111494

    Web of Science

    Scopus

  • Modified wavenumber and aliasing errors of split convective forms for compressible flows Reviewed

    Yuichi Kuya, Soshi Kawai

    Journal of Computational Physics   464   111336-1 - 111336-26   2022.9   ISSN:0021-9991 eISSN:1090-2716

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    Authorship:Lead author, Corresponding author   Publishing type:Research paper (scientific journal)   Publisher:Journal of Computational Physics  

    The spectral characteristics of split convective forms for compressible flows in finite difference methods are studied. It has been widely argued that the split forms are capable of reducing aliasing errors, based on the studies that consider spectral methods. However, the theoretical analysis shown here reveals that the split forms do not reduce aliasing errors in finite difference methods but rather increase aliasing errors more than the divergence form. This is because the modified wavenumber of the split forms may not become zero at the Nyquist wavenumber and is larger than that of the divergence form in the high wavenumber range. Correspondingly, this study also concludes that the superior numerical stability of kinetic energy preserving or kinetic energy and entropy preserving schemes, in which the split forms are used, is due to the enhanced preservation property of the kinetic energy and entropy and not the reduction of aliasing errors in finite difference methods. The spectral characteristics shown in the numerical tests are in good agreement with the theoretical analysis performed in this study.

    DOI: 10.1016/j.jcp.2022.111336

    Web of Science

    Scopus

  • A Prismatic Grid Generation Method Suitable for Predicting Aerodynamic Characteristics of Winged Re-entry Vehicles Reviewed

    Yasuhito Okano, Yuichi Kuya, Keisuke Sawada, Hideyuki Tanno

    JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES   70 ( 5 )   152 - 161   2022   ISSN:1344-6460 eISSN:2432-3691

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    Publishing type:Research paper (scientific journal)   Publisher:Japan Society for Aeronautical and Space Sciences  

    DOI: 10.2322/jjsass.70.152

  • High-order accurate kinetic-energy and entropy preserving (KEEP) schemes on curvilinear grids Reviewed

    Y. Kuya, S. Kawai

    Journal of Computational Physics   442   110482-1 - 110482-35   2021.10

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    Authorship:Lead author, Corresponding author  

    DOI: 10.1016/j.jcp.2021.110482

  • Numerical study of flowfield around a multislotted high-lift wing Reviewed

    Y. Kuya, R. Ito, M. Maki, K. Sawada

    Journal of Aircraft   58 ( 2 )   383 - 389   2021.3

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    Authorship:Lead author, Corresponding author  

    DOI: 10.2514/1.C035809

  • Preventing spurious pressure oscillations in split convective form discretization for compressible flows Reviewed

    N. Shima, Y. Kuya, Y. Tamaki, S. Kawai

    Journal of Computational Physics   427   110060-1 - 110060-10   2021.2

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  • Numerical study of transonic shock buffet control over a supercritical airfoil Reviewed

    Y. Kuya, K. Boda, K. Sawada

    Journal of Aircraft   57 ( 6 )   1242 - 1251   2020.11

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    Authorship:Lead author, Corresponding author  

    DOI: 10.2514/1.C035902

  • Physics and modeling of trailing-edge stall phenomena for wall-modeled large-eddy simulation Reviewed

    Y. Tamaki, Y. Fukushima, Y. Kuya, S. Kawai

    Physical Review Fluids   5   074602-1 - 074602-20   2020.7

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  • A stable and non-dissipative kinetic energy and entropy preserving (KEEP) scheme for non-conforming block boundaries on Cartesian grids Reviewed

    Y. Kuya, S. Kawai

    Computers & Fluids   200   104427-1 - 104427-20   2020.3

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    Authorship:Lead author, Corresponding author  

    DOI: 10.1016/j.compfluid.2020.104427

  • 動径基底関数を用いた遷音速フラッタ境界の高速予測法の研究 Reviewed

    澤木悠太, 久谷雄一, 澤田惠介

    航空宇宙技術   18   133 - 141   2019.7

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  • ハイブリッド非構造格子に対するスペクトラルボリューム法の格子収束性に関する研究 Reviewed

    澤木悠太, 久谷雄一, 澤田惠介

    航空宇宙技術   18   9 - 18   2019.1

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  • Kinetic energy and entropy preserving schemes for compressible flows by split convective forms Reviewed

    Y. Kuya, K. Totani, S. Kawai

    Journal of Computational Physics   375   823 - 853   2018.12

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    Authorship:Lead author, Corresponding author  

    DOI: 10.1016/j.jcp.2018.08.058

  • Multifidelity surrogate modeling of experimental and computational aerodynamic data sets Reviewed

    Y. Kuya, K. Takeda, X. Zhang, A. I. J. Forrester

    AIAA Journal   49 ( 2 )   289 - 298   2011.2

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    Authorship:Lead author, Corresponding author  

    DOI: 10.2514/1.J050384

  • Computational investigation of a race car wing with vortex generators in ground effect Reviewed

    Y. Kuya, K. Takeda, X. Zhang

    Journal of Fluids Engineering   132 ( 2 )   021102-1 - 021102-8   2010.2

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    Authorship:Lead author, Corresponding author  

    DOI: 10.1115/1.4000741

  • Flow separation control on a race car wing with vortex generators in ground effect Reviewed

    Y. Kuya, K. Takeda, X. Zhang, S. Beeton, T. Pandaleon

    Journal of Fluids Engineering   131 ( 12 )   121102-1 - 121102-8   2009.12

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    Authorship:Lead author, Corresponding author  

    DOI: 10.1115/1.4000420

  • Flow physics of a race car wing with vortex generators in ground effect Reviewed

    Y. Kuya, K. Takeda, X. Zhang, S. Beeton, T. Pandaleon

    Journal of Fluids Engineering   131 ( 12 )   121103-1 - 121103-9   2009.12

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    Authorship:Lead author, Corresponding author  

    DOI: 10.1115/1.4000423

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MISC

Professional Memberships

  • American Physical Society (APS)

    2024.7 - Present

  • 情報処理学会 (量子ソフトウェア研究会)

    2024.4 - Present

  • 日本流体力学会

    2020.2 - Present

  • The Japan Society for Aeronautical and Space Sciences

    2017.4 - Present

  • American Institute of Aeronautics and Astronautics (AIAA)

    2009.4 - Present

Committee Memberships

  • 日本航空宇宙学会   空力部門幹事  

    2025.4 - Present   

  • 日本航空宇宙学会   会誌編集委員  

    2024.4 - 2025.3   

  • 日本航空宇宙学会   空力部門委員  

    2024.4 - 2025.3   

  • 日本航空宇宙学会   北部支部幹事  

    2024.4 - 2025.3   

  • 日本流体力学会 年会2024   主幹事  

    2023.5 - 2024.9   

Research Projects

  • 量子機械学習による流体解析の加速 -流体画像計測の超解像-

    Grant number:25H00712  2025.4 - 2028.3

    日本学術振興会  科学研究費助成事業 基盤研究(A) 

    久谷 雄一

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    Authorship:Principal investigator  Grant type:Scientific research funding

  • 量子コンピュータを用いた収束計算を必要としない近似流体計算

    Grant number:JPMJFR2342  2024.10 - 2032.3

    国立研究開発法人科学技術振興機構(JST)  創発的研究支援事業 

    久谷 雄一

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    Grant type:Competitive funding other than Grants-in-Aid for Scientific Research

  • 量⼦アニーリングによる空⼒形状ブラックボックス最適化

    Grant number:J240001504  2024.6 - 2025.3

    JAXA  JAXA 航空イノベーションチャレンジ2024 

    久谷 雄一 

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    Authorship:Principal investigator  Grant type:Contract research

  • 量子アニーリングコンピュータに実装可能な流体計算アルゴリズムの構築

    Grant number:22K04530  2022.4 - 2025.3

    日本学術振興会   科学研究費助成事業 基盤研究(C) 

    久谷 雄一

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    Authorship:Principal investigator  Grant type:Scientific research funding

    次世代のコンピュータと称される量子コンピュータによる流体計算の実現は学術界だけでなく産業界においても期待されている.しかし,量子コンピュータがまともな流体計算に応用された例は未だない.量子コンピュータの中でも量子アニーリングコンピュータはすでに実用化されているが0と1の二値のみを扱う組合せ最適化問題に特化したマシンとなっているため,量子アニーリングコンピュータに対する流体計算アルゴリズムは未だ提案されていない.そこで本研究では,量子アニーリングコンピュータに実装可能な流体計算アルゴリズムを構築し,実際に量子アニーリングコンピュータ上で流体計算を行うことを目指す.

    CiNii Research

  • 数理モデルに基いた流れ場の種類によらない新しい層流-乱流遷移CFDモデルの構築

    Grant number:18K04556  2018.4 - 2021.3

    日本学術振興会  科学研究費助成事業 基盤研究(C) 

    久谷 雄一

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    Authorship:Principal investigator  Grant type:Scientific research funding

Class subject

  • 力学基礎

    2025.4 - Present   First semester

  • 高速気体力学

    2025.4 - Present   Second semester