SATO Makoto
| School of Advanced Engineering Department of Mechanical Science and Engineering | Associate Professor |
Career
Educational Background
Affiliated academic society
IDs
Identifiers
研究者番号：50648897
researchmap会員ID：B000330257
J-Global ID：201801005845701750
Research Field
Research Keyword
Paper
- Influence of Side Wall on Aerodynamic Characteristics of Single Rotor for Mars Helicopters
Hiroshi Yukita; Yuriko Shiratsuchi; Kota Yoshikawa; Ryutaro Onishi; Makoto Sato
International Journal of Computational Fluid Dynamics, 02 Jul. 2025, [Reviewed] - Spatial arrangement of vortex-generator-type plasma actuator for separation control of airfoil flow
Makoto Sato
Physics of Fluids, 01 Jan. 2025, [Reviewed] - MICRO-SIZE MARS AIRPLANE FOR THE STEPWISE MARS LANDING EXPLORATION PROGRAM
Yuriko Shiratsuchi; Kento Kaneko; Shion Okada; Akira Oyama; Kazuhiko Yamada; Hiroto Tanaka; Makoto Sato
ICAS 2024, Sep. 2024 - Large-Eddy-Simulations on Dynamic Stall Control Using Plasma Actuators at Reynolds Number of 1.0×10^6
Makoto Sato; Kenichi Takahama
AIAA AVIATION FORUM AND ASCEND 2024, 27 Jul. 2024 - Numerical Investigation on Interaction Between Wing and Propeller Installed in Close Proximity to Both Upper and Lower Surfaces of Wing
Ryu Moriya; Yoshiki Nakaniida; Shusuke Honda; Makoto Sato; Eiji Shima
AIAA AVIATION FORUM AND ASCEND 2024, 27 Jul. 2024 - Numerical Study on Aerodynamic Characteristics of Loop Propeller Toward Quiet eVTOL
Yoshiki Nakaniida; Makoto Sato; Eiji Shima
AIAA AVIATION FORUM AND ASCEND 2024, 27 Jul. 2024 - Dynamic Stall Control Using Spanwise-Type and Vortex-Generator-Type Plasma Actuators Around Pitching Airfoil
Kenichi Takahama; Makoto Sato; Hiroaki Fukumoto
AIAA AVIATION FORUM AND ASCEND 2024, 27 Jul. 2024 - Comparison of Separation Control Mechanisms for Synthetic Jet and Plasma Actuators
Yoshiaki Abe; Taku Nonomura; Makoto Sato; Hikaru Aono; Kozo Fujii
Actuators, Aug. 2023, [Reviewed] - Separation Control using Vortex-Generator-Type Plasma Actuator over Wide Reynolds Number Range
Shota Mayahara; Makoto Sato
AIAA AVIATION 2023 Forum, 08 Jun. 2023 - Numerical Investigation on Flow Field and Aerodynamic Characteristics of Box Wing for New Convertible eVTOL
Shusuke Honda; Makoto Sato; Nishida Ryoma; Eiji Shima
AIAA AVIATION 2023 Forum, 08 Jun. 2023 - Compressibility Effects on Aerodynamic Characteristics and Flow Fields of Mars Helicopter Rotor
Kota Yoshikawa; Yuta Buto; Makoto Sato; Akira Oyama; Masahiko Sugiura; Yasutada Tanabe; Keita Kimura; Kuniyuki Takekawa; Yuki Kishi; Masahiro Kanazaki
AIAA AVIATION 2023 Forum, 08 Jun. 2023 - Computational Study of the Plasma Actuator Flow Control for an Airfoil at Pre-Stall Angles of Attack
Takuto Ogawa; Kengo Asada; Makoto Sato; Tomoaki Tatsukawa; Kozo Fujii
Applied Sciences, 09 Sep. 2022, [Reviewed] - AERODYNAMIC CHARACTERISTICS OF BOX WINGS FOR AN INNOVATIVE EVTOL CONFIGURATION
E. SHIMA; K. YONEZAWA; R. NISHIDA; S. HONDA; M. SATO
ICAS 2022, Sep. 2022 - Sound source characteristics generated by shocklets in isotropic compressible turbulence
Daiki Terakado; Taku Nonomura; Soshi Kawai; Hikaru Aono; Makoto Sato; Akira Oyama; Kozo Fujii
Physical Review Fluids, 19 Aug. 2022, [Reviewed] - Numerical investigation on streamwise vortex generation by plasma actuator
Makoto Sato
Physics of Fluids, 01 Aug. 2022, [Reviewed] - Mechanisms for Turbulent-Separation-Control at Reynolds Number of 1.6×106 using Vortex-Generator-Type Plasma Actuators - Comparison with Spanwise-Type Plasma Actuators
Makoto Sato
AIAA AVIATION 2022 Forum, 20 Jun. 2022 - Numerical Analysis on Hovering Performance of Hexacopter “HAMILTON” for Mars Exploration
Yuki Kishi; Masahiro Kanazaki; Masahiko Sugiura; Yasutada Tanabe; Akira Oyama; Makoto Sato
AIAA AVIATION 2022 Forum, 20 Jun. 2022 - Blade Shape Optimization of Mars Helicopter Exploring Pit Craters
Masahiko Sugiura; Masahiro Kanazaki; Makoto Sato; Takuma Minajima; Keita Kimura; Akira Oyama; Hideaki Sugawara; Yasutada Tanabe; Yuki Kishi; Daisuke Kikuchi; Kota Yoshikawa; Yuta Buto; Takuma Minajima
Proceedings of the Vertical Flight Society 78th Annual Forum, 10 May 2022 - Separated flow control of small horizontal-axis wind turbine blades using dielectric barrier discharge plasma actuators
Hikaru Aono; Hiroaki Fukumoto; Yoshiaki Abe; Makoto Sato; Taku Nonomura; Kozo Fujii
Energies, 01 Mar. 2020, [Reviewed] - Unified mechanisms for separation control around airfoil using plasma actuator with burst actuation over Reynolds number range of 103-106
Makoto Sato; Koichi Okada; Kengo Asada; Hikaru Aono; Taku Nonomura; Kozo Fujii
Physics of Fluids, 01 Feb. 2020, [Reviewed] - Mechanisms for turbulent separation control using plasma actuator at Reynolds number of 1.6 × 10^6
Makoto Sato; Kengo Asada; Taku Nonomura; Hikaru Aono; Aiko Yakeno; Kozo Fujii
Physics of Fluids, 01 Sep. 2019, [Reviewed] - Plasma-Actuator Burst-Mode Frequency Effects on Leading-Edge Flow-Separation Control at Reynolds Number 2.6×105
Hikaru Aono; Soshi Kawai; Taku Nonomura; Makoto Sato; Kozo Fujii; Koichi Okada
AIAA Journal, Nov. 2017, [Reviewed] - Experimental Study on the Detailed Structure of Separation Bubble in Flow Control with DBD Plasma Actuator
Yuma Miyakawa; Satoshi Sekimoto; Makoto Sato; Taku Nonomura; Akira Oyama; Kozo Fujii; Shinichiro Ito
47th AIAA Fluid Dynamics Conference, 02 Jun. 2017 - Large-Eddy Simulation of NACA 0015 Airfoil Flow at Reynolds Number of 1.6×10^6
Makoto Sato; Kengo Asada; Taku Nonomura; Soshi Kawai; Kozo Fujii
AIAA Journal, Feb. 2017, [Reviewed] - Development of a compressible flow solver using hierarchical Cartesian grids --toward the age of Exa-scale supercomputers--
H. Shibata; M. Sato; Y. Fukushima; S. Tsutsumi; T. Nonomura; S. Kawai; R. Takaki
Parallel CFD Conference 2017, 2017 - Adapting High Resolution PIV to Shear Layer on Flow Controlled by DBD Plasma Actuator
Y. Miyakawa; S. Sekimoto; M. Sato; T. Nonomura; A. Oyama; K. Fujii; S. Ito
The Ninth JSME-KSME Thermal and Fluids Engineering Conference, 2017 - Control of Airfoil Flow at Cruise Condition by DBD Plasma Actuator - Sophisticated Airfoil vs. Simple Airfoil with Flow Control -
Kento Asano; Makoto Sato; Taku Nonomura; Akira Oyama; Kozo Fujii
8th AIAA Flow Control Conference, 10 Jun. 2016 - Mechanisms for laminar separated-flow control using dielectric-barrier-discharge plasma actuator at low Reynolds number
Makoto Sato; Taku Nonomura; Koichi Okada; Kengo Asada; Hikaru Aono; Aiko Yakeno; Yoshiaki Abe; Kozo Fujii
Physics of Fluids, 01 Nov. 2015, [Reviewed] - Multifactorial Effects of Operating Conditions of Dielectric-Barrier-Discharge Plasma Actuator on Laminar-Separated-Flow Control
Makoto Sato; Hikaru Aono; Aiko Yakeno; Taku Nonomura; Kozo Fujii; Koichi Okada; Kengo Asada
AIAA Journal, Sep. 2015, [Reviewed] - Contribution of large-scale vortex and fine-scale turbulent structure in separated flow control using DBD plasma actuator
Kento Asano; Kengo Asada; Hiroki Kato; Makoto Sato; Taku Nonomura; Kozo Fujii
45th AIAA Fluid Dynamics Conference, 18 Jun. 2015 - LES of transient flows controlled by DBD plasma actuator over a stalled airfoil
K. Asada; T. Nonomura; H. Aono; M. Sato; K. Okada; K. Fujii
International Journal of Computational Fluid Dynamics, 16 Mar. 2015, [Reviewed] - LES of Separated-flow Controlled by DBD Plasma Actuator around NACA 0015 over Reynolds Number Range of 10^4-10^6
Makoto Sato; Koichi Okada; Hikaru Aono; Kengo Asada; Aiko Yakeno; Taku Nonomura; Kozo Fujii
53rd AIAA Aerospace Sciences Meeting, 03 Jan. 2015 - RELATION BETWEEN SOUND SOURCES AND VORTICAL STRUCTURES IN ISOTROPIC COMPRESSIBLE TURBULENCE
Daiki Terakado; Taku Nonomura; Makoto Sato; Kozo Fujii
PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, 2014, VOL 7, 2015, [Reviewed] - Computational and experimental analysis of flow structures induced by a plasma actuator with burst modulations in quiescent air
Aono, Hikaru; Sekimoto, Satoshi; Sato, Makoto; Yakeno, Aiko; Nonomura, Taku; Fujii, Kozo
MECHANICAL ENGINEERING JOURNAL, 2015, [Reviewed] - Effective Mechanisms for Turbulent-separation Control by DBD Plasma Actuator around NACA0015 at Reynolds Number 1,600,000
Makoto Sato; Kengo Asada; Taku Nonomura; Hikaru Aono; Aiko Yakeno; Kozo Fujii
7th AIAA Flow Control Conference, 13 Jun. 2014 - LES on Turbulent Separated Flow around NACA0015 at Reynolds Number 1,600,000 toward Active Flow Control
Kengo Asada; Makoto Sato; Taku Nonomura; Soshi Kawai; Hikaru Aono; Aiko Yakeno; Kozo Fujii
32nd AIAA Applied Aerodynamics Conference, 13 Jun. 2014 - Effects of Burst Frequency and Momentum Coefficient of DBD Actuator on Control of Deep-stall Flow around NACA0015 at Rec=2.6x10^{5}
Hikaru Aono; Koichi Okada; Taku Nonomura; Soshi Kawai; Makoto Sato; Aiko Yakeno; Kozo Fujii
52nd Aerospace Sciences Meeting, 10 Jan. 2014 - Flow Control using a DBD Plasma Actuator for Horizontal-axis Wind Turbine Blades of Simple Experimental Model
Hikaru Aono; Yoshiaki Abe; Makoto Sato; Aiko Yakeno; Koichi Okada; Taku Nonomura; Kozo Fujii
11th World Congress on Computational Mechanics, WCCM 2014, 5th European Conference on Computational Mechanics, ECCM 2014 and 6th European Conference on Computational Fluid Dynamics, ECFD 2014, 2014, [Reviewed] - Compressibility effects on sound source distributions in isotropic compressible turbulence
D. Terakado; T. Nonomura; M. Sato; K. Fujii
10th International ERCOFTAC Symposium on Engineering Turbulence Modelling and Measurements, 2014 - Visualization of Momentum Added/Induced by a Plasma Actuator Controlling Separated Flow Over An Airfoil
T. Nonomura; M. Sato; K. Okada; H. Aono; A. Yakeno; K. Fujii
The 16th International Symposium on Flow Visualization, 2014 - CONTROL OF LAMINAR SEPARATION IN VARIOUS AIRFOILS BY DBD PLASMA ACTUATOR
Makoto Sato; Koichi Okada; Hikaru Aono; Aiko Yakeno; Taku Nonomura; Kozo Fujii
Jets, wakes and separated flows : proceedings of International Conference on Jets, Wakes and Separated Flows, ICJWSF, 16 Sep. 2013 - Massive Parametric Study by LES on Separated-flow Control around Airfoil using DBD Plasma Actuator at Reynolds Number 63,000
Makoto Sato; Koichi Okada; Taku Nonomura; Hikaru Aono; Aiko Yakeno; Kengo Asada; Yoshiaki Abe; Kozo Fujii
43rd Fluid Dynamics Conference, 22 Jun. 2013 - Significance of Three-dimensional Unsteady Flows inside the Cavity on Separated-flow Control around an NACA0015 using a Synthetic Jet
Yoshiaki Abe; Koichi Okada; Makoto Sato; Taku Nonomura; Kozo Fujii
43rd Fluid Dynamics Conference, 22 Jun. 2013 - Control Mechanism of Plasma Actuator for Separated Flow around NACA0015 at Reynolds Number 63,000 -Separation Bubble Related Mechanisms-
Taku Nonomura; Hikaru Aono; Makoto Sato; Aiko Yakeno; Koichi Okada; Yoshiaki Abe; Kozo Fujii
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 05 Jan. 2013 - Direct Numerical Simulation of Ignition and Propagation of H2/Air, CH4/Air and n-Heptane/Air Premixed Mixture in Turbulence
M. Sato; S. Matsuura; M. Tanahashi; T. Miyauchi
Proceedings of the 2nd International Forum on Heat Transfer, 2008 - Direct Numerical Simulation of Ignition and Propagation of Turbulent H2/Air, CH4/Air and n-Heptane/Air Premixed Flames
M. Sato; S. Matsuura; M. Tanahashi; T. Miyauchi
International Symposium on Advances in Computational Heat Transfer, 2008 - DNS of Turbulent Premixed Flames Propagating along Isothermal Wall
A. Tsunemi; S. Matsuura; M. Sato; M. Tanahashi; T. Miyauchi; M. Nagaoka
Proceedings of the 7th JSME-KSME Thermal and Fluids Engineering Conference, 2008 - Particle Dispersion and Coherent Fine Scale Eddies in Turbulence
M. Sato; M. Tanahashi; T. Miyauchi
Journal of Fluid Science and Technology, 2008, [Reviewed] - Huge Direct Numerical Simulation of Turbulent Combustion - Toward Perfect Simulation of IC Engine –
M. Tanahashi; T. Seo; M. Sato; A. Tsunemi; T. Miyauchi
Journal of Computational Fluids Engineering, 2008, [Reviewed] - Particle dispersion in fine scales of homogeneous isotropic turbulence
M. Sato; M. Tanahashi; T. Miyauchi
FEDSM 2007: PROCEEDINGS OF THE 5TH JOINT AMSE/JSME FLUIDS ENGINEERING SUMMER CONFERENCE VOL 1, PTS A AND B, 2007 - Fractal Geometry and Mixing Transition in Turbulent Mixing Layer
M. Tanahashi; Y. Wang; T. Fujisawa; K. Chinda; M. Sato; T. Miyauchi
Proceedings of the 5th International Symposium on Turbulence and Shear Flow Phenomena, 2007 - Droplet Dispersion and Vapor Mixing by Fine Scale Turbulence
M. Sato; M. Tanahashi and T. Miyauchi
Proceedings of 5th International Symposium on Turbulence, Heat and Mass Transfer, 2006
MISC
- Mechanisms for Airfoil Separation Control using Plasma Actuator,- Unified Knowledge from High-Fidelity Numerical Simulations-
M. Sato; H. Aono
nagare, 2020, [Invited]
Lead - ボルテックスジェネレータ型プラズマアクチュエータを用いたNACA4418周り流れの剥離制御メカニズム
佐藤允; 佐藤允; 野々村拓; 青野光
日本機械学会年次大会講演論文集(CD-ROM), 02 Sep. 2017 - 流体制御を利用した輸送システム・流体機器設計概念の革新を目指して －「京」利用による流れ現象理解と制御パラメータの発見－
2015 - 革新的流体制御技術の研究開発「「京」大規模計算によるマイクロデバイス流体制御」
2014 - DBDプラズマアクチュエータを用いた翼剥離制御の大規模パラメトリックスタディ
2013 - DNS and Combined Laser Diagnostics of Turbulent Combustion
Mamoru Tanahashi; Makoto Sato; Masayasu Shimura; Toshio Miyauchi
JOURNAL OF THERMAL SCIENCE AND TECHNOLOGY, 2008 - 乱流熱物質輸送現象の超大規模直接数値計算
2006
Lectures, oral presentations, etc.
- 渦突風と翼の干渉流れに対する各種PAを用いた流体制御
Jan. 2025 - Large-eddy simulation on laminar-separation-bubble affected by swirling flow simulating propeller slipstream for low Reynolds number airfoil flow
Akito Goto; Makoto Sato
77th Annual Meeting of the Division of Fluid Dynamics, Nov. 2024 - 剛体翼を用いた超小型火星飛行機の設計検討
Nov. 2024 - プラズマアクチュエータを用いたバーチャルボルテックスジェネレータが生成する渦構造の解明
Nov. 2024 - 推進効率を向上した有翼eVTOLにおけるプロペラと主翼の空力干渉
Oct. 2024 - 低レイノルズ数・Pre-Stall翼周り流れにおける ボルテックスジェネレータ型PAを用いた流体制御
Sep. 2024 - 火星ヘリコプタ用ロータの壁面近傍における空力特性
Jul. 2024 - PPB型eVTOLおよび静粛ロータ「Looprop」に関する数値解析
Mar. 2024 - PAを用いた動的翼周り流れの流体制御におけるレイノルズ数効果
25 Nov. 2023 - プラズマアクチュエータの間欠駆動による流体制御 -数値解析の見地から-
25 Nov. 2023 - 翼に近接するプロペラを持つ有翼eVTOLにおけるガーニーフラップの効果について
16 Nov. 2023 - 有翼eVTOLにおけるプロペラ回転方向の影響
15 Nov. 2023 - PPB型eVTOLにおけるプロペラ-Box翼の空力特性
15 Nov. 2023 - 新しい転換型eVTOLにおけるプロペラ-翼干渉に関する数値解析
04 Nov. 2023 - 低レイノルズ数流れにおける翼の高揚力装置に関する数値的研究
04 Nov. 2023 - 実風車スケールの動的な翼周り流れにおけるスマートな剥離制御技術の実証
25 Oct. 2023 - 火星ヘリコプタの実現に向けた遷音速ロータの空力特性に関する研究
17 Oct. 2023 - 低レイノルズ数流れとなる火星サンプルリターンロケットの空力特性に関する研究
17 Oct. 2023 - 高レイノルズ数の動的翼周り流れにおける各種プラズマアクチュエータを用いた乱流剥離制御
04 Sep. 2023 - ピッチング翼周りの動的失速流れ制御,におけるプラズマアクチュエータの配置
12 Jul. 2023 - プロペラを模擬した旋回流が翼面上の層流剥離泡に与える影響
12 Jul. 2023 - 静粛ロータ「Looprop」の遷音速特性に関するCFD解析
12 Jul. 2023 - 火星ヘリコプタ「HAMILTON」に関する数値解析および計測実験
24 Mar. 2023 - 火星環境下でのロケットの空力設計に関する研究
01 Nov. 2022 - 実⾵⾞スケールの翼周り流れにおけるスマートな剥離制御技術の実証
27 Oct. 2022 - ボルテックスジェネレータ型PAを用いた翼周り剥離制御効果におけるレイノルズ数依存性
12 Oct. 2022 - 火星ヘリコプタ用ロータの翼型による空力特性の比較検証
12 Oct. 2022 - Box翼特有のサイドウイングが空力特性に与える影響
12 Oct. 2022 - Box翼VTOLの遷移飛行における空力特性
12 Oct. 2022 - Separation Control around Airfoil Flow under Low Reynolds Number Conditions using Vortex-Generator Type Plasma Actuator
29 Jun. 2022 - CFD analysis on Flow and Aerodynamic Characteristics around Box Wing for Low-Noise eVTOL
29 Jun. 2022 - Experimental Measurement and Numerical Simulation on Aerodynamic Characteristics of the rotor in Martian Helicopter "HAMILTON"
29 Jun. 2022 - 火星地下空洞探査を目的とした火星ヘリコプターに関する取り組み
08 Apr. 2022, [Invited] - 火星ヘリコプタ『HAMILTON』に関する数値解析
Mar. 2022 - 風車の翼周りの流れを模擬した動的流れ場における各種PAの剥離制御効果
17 Jan. 2022 - ボルテックスジェネレータ型PAの連続駆動による翼周り剥離制御に関するレイノルズ数効果
17 Jan. 2022 - 火星地下空洞探査を実現するヘリコプタの空力研究紹介
12 Nov. 2021 - 高レイノルズ数流れにおけるスパン型およびボルテックスジェネレータ型プラズマアクチュエータを併用した高効率でロバストな剥離制御
29 Oct. 2021 - Turbulent Separation Control of Airfoil Flow at Reynolds Number of 1,600,000 using Vortex-Generator Type PA
08 Sep. 2021 - Mach Number Effects on Rotor Performance of Martian Helicopter "HAMILTON"
01 Jul. 2021 - Numerical Investigation of Aerodynamic Characteristics around Hexacopter “HAMILTON” for Martian Exploration Using Moving Overlapped Grid
01 Jul. 2021 - Separation Control around NACA0015 Airfoil using Vortex Generator Type Plasma Actuator over Low Reynolds Number Conditions
S. Mayahara; M. Sato
ISAT-20, 2021 - レイノルズ数変化に伴う三角厚翼ロータの空力・流れ場特性の評価
14 Dec. 2020 - BOX 翼を持つマルチコプタの風洞実験(第 2 報)
27 Nov. 2020 - 三角厚翼ブレードのレイノルズ数効果に関する数値的研究
25 Nov. 2020 - Study of Coaxial Inversion Rotor Aimed at Realizing Mars Helicopter (3)
H. Nagai; K. Fujita; A. Yamaguchi; A. Oyama; K. Yonezawa; K. Kitamura; Y. Furusawa; M. Sato; M. Kanazaki
17th International Conference on Flow Dynamics, 29 Oct. 2020 - 低レイノルズ数環境下における三角厚翼ローターの数値的研究
27 Oct. 2020 - Wind Tunnel Testing of a Multicopter with Box Wing
29 Sep. 2020 - Aerodynamic Optimal Design of Mars Helicopter Rotor Blade Planform
29 Sep. 2020 - Comparison of rotor characteristics between early type Looprop and straight blade
29 Sep. 2020 - Numerical study on flow characteristics of a circulation control wing installed in two plane plates
18 Sep. 2020 - Effects of location and operating conditions of vortex-generator type PA on separation control around airfoil – Second Report –
15 Sep. 2020 - Numerical simulation of a rotating blade using a flat-plate airfoil at low Reynolds numbers for Mars helicopter
D. Ogasawara; M. Sato; H. Sugawara; Y. Tanabe; K. Sato
72nd Annual Meeting of the American Physical Society Division of Fluid Dynamics, 23 Nov. 2019 - On spatial arrangement of vortex-generator type plasma actuator for separation control of,airfoil flow
M. Sato; C. Kobayashi
72nd Annual Meeting of the American Physical Society Division of Fluid Dynamics, 23 Nov. 2019 - Effects of location and operating conditions of vortex-generator type PA on separation control around airfoil
09 Sep. 2019 - Numerical Study on flow field of drone rotor “Looprop” using rFlow3D
01 Jul. 2019 - Numerical study on rotating flat airfoil under low Reynolds number condition using rFlow3D
01 Jul. 2019 - Numerical simulation on rotational flat-plate-airfoil flow using rFlow3D
Diachi Ogasawara; Makoto Sato; Yasutada Tanabe; Hideaki Sugawara
1st Symposium on Mars Helicopter, 11 Mar. 2019 - ボルテックジェネレータ型PAの設計・駆動条件の影響
15 Nov. 2018 - PIV analysis for transient period of separation control around airfoil with DBD plasma actuator
中村開人,Hasse Dekker,下村伶,関本諭志,佐藤允,大山聖,藤井孝藏
第6回プラズマアクチュエータ研究会シンポジウム, 15 Nov. 2018 - Separated-flow control around airfoil using vortex-generator type plasma actuator and spanwise type plasma actuator
09 Sep. 2018 - Wall-resolved LES on large-wind-turbine blade-element flow at Reynolds number of 3*10^6
Makoto Sato; Kengo Asada; Taku Nonomura; Hikaru Aono
35th ANSS, 29 Jun. 2017, The Japan Society for Aeronautical and Space Sciences Aerodynamics Division Committee - 階層型直交格子法における流束ベース壁面境界条件の検討
Toshikazu Shibata; Makoto Sato; Seiji Tsutsumi; Yuma Fukushima; Taku Nonomura; Soshi Kawai; Ryoji Takagi
第49回流体力学講演会／第35回航空宇宙数値シミュレーション技術シンポジウム, 29 Jun. 2017 - Mechanism of separated-flow control around NACA4418 using vortex-generator type plasma actuator
M. Sato; T. Nonomura; H. Aono
ISAT-16, 2017 - ボルテックスジェネレータ型プラズマアクチュエータを用いたNACA4418周り流れの剥離制御メカニズム
2017 - 階層型直交格子を用いた圧縮性流体ソルバの開発
Dec. 2016 - DBDプラズマアクチュエータとシンセティックジェットを用いた翼周り剥離流れの制御効果の比較
Dec. 2015 - 幅広いレイノルズ数におけるDBDプラズマアクチュエータを用いた翼周り剥離流れの制御
Dec. 2015 - 複数のプラズマアクチュエータを用いた翼周り剥離制御のLES
Sep. 2015 - 低レイノルズ数領域における高性能翼と剥離制御された単純翼の空力性能の比較
Sep. 2015 - マイクロデバイスを用いた輸送機器・流体機器の流体制御に関するLES
Sep. 2015, [Invited] - Control Mechanism of DBD Plasma Actuator for Deep-Stall Flows around NACA0015
H. Kato; M. Sato; H. Aono; A. Yakeno; T. Nonomura and K. Fujii
EDRFCM 2015, Mar. 2015 - 低レイノルズ数でのDBDプラズマアクチュエータを用いた翼剥離制御におけるバースト比効果
Mar. 2015 - Re10^4-10^6におけるDBDプラズマアクチュエータを用いた翼周り剥離制御のLES解析
Dec. 2014 - DBDプラズマアクチュエータを用いた翼周り剥離流れ制御における大規模渦構造と乱流微細構造の寄与 -2次元計算と3次元LES計算の比較-
Dec. 2014 - 一様等方性圧縮性乱流における音源項の統計的性質
Oct. 2014 - 高レイノルズ数におけるDBDプラズマアクチュエータを用いた翼周り乱流剥離制御のLES
Sep. 2014 - 2メーター直径3枚ブレード回転機器模型まわり剥離流れへのプラズマ気流制御効果に関する数値解析
Sep. 2014 - 一様等方性圧縮性乱流の音源分布
Jun. 2014 - マイクロデバイスを用いた輸送機器・流体機器の流体制御に関するLarge-eddy simulation
Mar. 2014 - Large-eddy simulation of a two-meter, three-bladed simple wind turbine model controlled by a plasma actuator
H. Aono; Y. Abe; M. Sato; A. Yakeno; K. Okada; T. Nonomura; K. Fujii
ICFD2014, 2014 - Separated-flow control by DBD plasma actuator around airfoils at Reynolds number 63,000
M. Sato; K. Okada; H. Aono; A. Yakeno; K. Asada; Y. Abe; T. Nonomura and K. Fujii
APCOM&ISCM, Dec. 2013 - シンセティックジェットによる翼周り剥離流れの制御に関するLES: スパン方向渦の解析
Dec. 2013 - レイノルズ数1,600,000における翼周りのLES: 乱流剥離とその制御
Dec. 2013 - LES of turbulent separated flow over NACA0015 at Reynolds number 1,600,000 --toward the separation control by a DBD plasma actuator
M. Sato; K. Asada; T. Nonomura; S. Kawai; H. Aono; A. Yakeno and K. Fujii
APS 66th Annual DFD Meeting 2013, Nov. 2013 - 中レイノルズ数でのDBDプラズマアクチュエータを用いた翼剥離制御におけるバースト発振周波数効果
Nov. 2013 - DBDプラズマアクチュエータを用いた翼周り剥離制御における翼形状の影響
Sep. 2013 - レイノルズ数260,000におけるDBDプラズマアクチュエータを用いたNACA0015翼の剥離制御LES解析
Sep. 2013 - Multi-Objective Design Exploration of DBD Plasma Actuator for Low Reynolds Number Application
T. Sulaiman; S. Sekimoto; M. Sato; T. Nonomura; A. Oyama; K. Fujii
日本機械学会2013年度年次大会, Sep. 2013 - 回転する計算格子の下で幾何学的保存則を満足する高次精度差分スキームの提案
Jun. 2013 - DBDプラズマアクチュエータを用いた翼剥離制御に関する大規模パラメトリックスタディ
Dec. 2012 - DBDプラズマアクチュエータを用いた翼剥離流れ制御の非定常流れ場解析
Dec. 2012 - Parametric study on separation control by DBD plasma actuator over NACA0012 and NACA0015 airfoil at Reynolds number 63,000
M. Sato; T. Nonomura; H. Aono; K. Okada; K. Fujii
APS 65th Annual DFD Meeting 2012, Nov. 2012 - Fractal Geometry and Mixing Transition in Turbulent Free Shear Flow
M. Tanahashi; S. Ishimoto; M. Sato; T. Seo and T. Miyauchi
8th Sino-Japan Workshop on Turbulence, Apr. 2009 - Fine Scale Eddy Cluster and Hierarchical Structure in Homogeneous Isotropic Turbulence
T. Miyauchi; T. Kubota; M. Sato and M. Tanahashi
8th Sino-Japan Workshop on Turbulence, Apr. 2009 - Local and Global Flame Structures of H2/Air Turbulent Premixed Flames at High Reynolds Number
S. Tanaka; M. Sato; T. Seo; M. Tanahashi and T. Miyauchi
The 2nd International Forum on Multidisciplinary Education and Research Center for Energy Science, 2009 - 高Reynolds数水素・空気乱流予混合火炎の直接数値計算
Nov. 2008 - 高レイノルズ数一様等方性乱流の大規模直接数値計算による乱流構造の解明
Nov. 2008 - 高Reynolds数水素・空気乱流予混合火炎の局所火炎構造
Sep. 2008 - 高解像度Dual-Plane Stereoscopic PIV による乱流コヒーレント微細構造の計測
Sep. 2008 - 乱流微細構造と高シュミット数スカラー混合のフラクタル特性
Sep. 2008 - 高レイノルズ数一様等方性乱流の微細渦クラスターのスケーリング則
Sep. 2008 - 水素・空気，メタン・空気及びn-ヘプタン・空気乱流予混合気における着火と火炎伝播のDNS
May 2008 - 直接数値計算による乱流予混合火炎の壁面近傍挙動の解明
May 2008 - DNS of Ignition and Propagation of Turbulent H2/Air, CH4/Air and n-Heptane/Air Premixed Flames
M. Sato; S. Matsuura; M. Tanahashi and T. Miyauchi
12th International Conference on Numerical Combustion, Apr. 2008 - Scaling Law of Fine Scale Eddy Cluster in Homogeneous Isotropic Turbulence at High Reynolds Number
KUBOTA Taisuke; SATO Makoto; TANAHASHI Mamoru; MIYAUCHI Toshio
2008 - Measurement of Coherent Fine Scale Structure in Turbulence by High Resolution Dual-Plane Stereoscopic PIV
TANAHASHI Mamoru; HIRAYAMA Tetsu; SHIMURA Masayasu; SATO Makoto; MIYAUCHI Toshio
2008 - Local Flame Structure of High Reynolds Number H_2/Air Turbulent Premixed Flame
TANAKA Shoichi; SATO Makoto; TANAHASHI Mamoru; MIYAUCHI Toshio
2008 - Fine Scale Structure and Fractal Geometry of Scalar Mixing at High Schmidt Numbers in Turbulence
ISHIMOTO Sachinori; SATO Makoto; SEO Takehiko; TANAHASHI Mamoru; MIYAUCHI Toshio
2008 - E234 Direct Numerical Simulation of Ignition of n-Heptane/Air Mixture
SATO Makoto; TANAHASHI Mamoru; MIYAUCHI Toshio
Procee[d]ings of Thermal Engineering Conference, 23 Nov. 2007, The Japan Society of Mechanical Engineers - DNS によるn-ヘプタン・空気混合気の着火機構の解明
Nov. 2007 - コヒーレント微細渦の特性に基づく液滴分散及び蒸気混合機構の解明
Dec. 2006 - 乱流微細構造による蒸発液滴の分散及び蒸気混合機構
Sep. 2006 - ヘプタン・空気混合気の着火及び火炎伝播における化学反応モデルの検証”,
May 2006 - 一様等方性乱流中の液滴蒸発及び蒸気混合機構
May 2006 - Droplet Dispersion and Vapor Mixing by Coherent Fine Scale Structure of Turbulence
M. Sato; M. Tanahashi and T. Miyauchi
11th International Conference on Numerical Combustion, Apr. 2006 - 一様等方性乱流中の液滴蒸発機構
Dec. 2005 - Droplet Dispersion and Vapor Mixing by Fine Scale Turbulence
M. Sato; M. Tanahashi and T. Miyauchi
APS 58th Annual DFD Meeting 2005, Nov. 2005 - 一様等方性乱流中の蒸発液滴の分散機構
Sep. 2005 - トンネル内爆発事故時の爆風伝播解析
Mar. 2004
Award
Others
Research Themes
Member History
