Akira Oyama

(大山聖)

Profile Information

Affiliation: Professor, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
The University of Tokyo
Tokyo University of Science

Degree: Ph.D. in Engineering(Mar, 2000, Tohoku University)

Researcher number: 10373440
J-GLOBAL ID: 200901044748363926
researchmap Member ID: 5000069161

External link: https://ladse.eng.isas.jaxa.jp/

宇宙科学航空研究開発機構宇宙科学研究所の大山です．
自分の研究分野にとらわれず，新しい研究分野にも挑戦していきたいと考えています．

Research Interests

Research Areas

Research History

Dec, 2023 - Present

Professor, The Graduate School of Engineering, The University of Tokyo
Apr, 2023 - Present

Professor, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
Apr, 2019 - Present

Tokyo University of Science
Apr, 2015 - Nov, 2023

准教授, 工学系研究科, 東京大学大学院
Apr, 2010 - Mar, 2023

Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency

Education

Apr, 1997 - Mar, 2000

航空宇宙工学専攻博士課程, 工学研究科, 東北大学大学院
- 2000

Department of Aeronautivs and space Engieering, Graduate School, Division of Engineering, Tohoku University
Apr, 1995 - Mar, 1997

航空宇宙工学専攻修士課程, 工学研究科, 東北大学大学院
Apr, 1991 - Mar, 1995

Faculty of Engineering, Tohoku University
- 1995

Department of Aeronautics and Space Engineering, Faculty of Engineering, Tohoku University

Committee Memberships

Oct, 2020 - Present

監事, 進化計算学会
Jun, 2010 - Present

Intelligent Systems Technical Committee member, AIAA
Oct, 2018 - Sep, 2020

特任連携会員, 日本学術会議
Apr, 2017 - Mar, 2019

編集理事（会誌）, 日本航空宇宙学会
Apr, 2015 - Mar, 2017

計算力学部門総務委員会委員, 日本機械学会

Awards

Papers

143

Effect of the Riblet in the Transitional Flow Region

Kento Kaneko, Akira Oyama, Aiko Yakeno

JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 73(2) 33-41, 2025
Multiobjective Evolutionary Topology Optimization Algorithm Using Quadtree Encoding

Naruhiko Nimura, Akira Oyama

IEEE Access, 12 73839-73848, May, 2024 Peer-reviewedCorresponding author
Mach Number Effect on the Drag Reducing Performance of the Riblet in the Transition and Turbulent Flow

Kento Kaneko, Akira Oyama, Aiko Yakeno, Shingo Hamada

AIAA SciTech Forum and Exposition, 2024, 2024
Viscous Drag Reduction Effect of Riblet at Cruising Speed of Transonic Aircraft

Kento Kaneko, Akira Oyama, Aiko Yakeno

AIAA Aviation Forum and ASCEND, 2024, 2024
Development and Application of Three-Dimensional High-Degree-of-Freedom Multiobjective Design Optimization Method

Naruhiko Nimura, Akira Oyama

15(1) 20-30, Jan, 2024 Peer-reviewedCorresponding author

Misc.

月の縦孔・地下空洞を発見したSELENE「かぐや」地形カメラによる観測ならびにデータ解析技術

大山聖

日本航空宇宙学会誌, 72(7) 243-245, Jul, 2024 Invited
Development status of sub-scale flight test bed apllying ATRIUM engine

SAKAMOTO, Yuki, KOBAYASHI, Hiroaki, MARU, Yusuke, TOKUDOME, Shinichiro, OYAMA, Akira, TAKEUCHI, Shinsuke, MIURA, Masashi, MASAKI, Daisaku, TAKADA, Satoshi, KAKUDO, Hiromitsu, KAGA, Toru, YAMASHIRO, Ryoma, KINUFUCHI, Kiyoshi, MANAKO, Hiroyasu, UCHIUMI, Masaharu, NAKATA, Daisuke, EGUCHI, Hikaru, MINATO, Ryojiro, FUKIBA, Katsuyoshi, KAWASAKI, Akira, MAEDA, Shinichi, TAKEDA, Yoichi, SATO, Tetsuya

Proceedings of Sounding Rocket Symposium 2023, Feb, 2024

誤記: NAKATA, Dasuke
Conceptual Study of Reusable Rocket utilizing the Earth’s Atmosphere

丸祐介, 小林弘明, 大山聖, 坂本勇樹, 徳留真一郎, 佐藤哲也

日本機械学会年次大会講演論文集(CD-ROM), 2024, 2024
Multi-objective design optimization of a box fan for improving static pressure head and sound pressure level

中村幸太郎, 小泉拓, 山出吉伸, 岩瀬拓, 十川直幸, 川鍋友宏, 磯野勝朝, 大山聖, 金子公寿, 加藤千幸

みずほリサーチ&テクノロジーズ技報(Web), 3(1), 2024
System Analysis of Reusable Sounding Rocket with the ATRIUM engine

丸祐介, 佐藤哲也, 小林弘明, 大山聖, 坂本勇樹

航空原動機・宇宙推進講演会講演論文集(CD-ROM), 63rd, 2024

Books and Other Publications

Constraint-handling in evolutionary aerodynamic design

Akira Oyama

Springer Verlag, 2009 Refereed

Presentations

399

Numerical Simulation of Dynamic Derivatives for Mars Airplane Balloon Experiment-2 (MABE-2)

Masahiro Kanazaki, H Kittaka, Akira Oyama, Koji Fujita, Hiroki Nagai

The 16th International Conference on Flow Dynamics, Nov, 2019
Aeroelastic Deformation Measurement of Mars Airplane for High-Altitude Flight Experiment Using Stereo Photogrammetry Technique

Syuichi Hiramatsu, Masayuki Anyoji, Koji Fujita, Hiroki Nagai, Akira Oyama, Hiroyuki Kato

the 11th International Meeting on Advances in ThermoFluids, Nov, 2019
Wind Tunnel Test for Videogrammetric Deformation Measurement of UAV for Mars Airplane Balloon Experiment-1 (MABE-1)

Koji Fujita, Akira Oyama, Daisuke Kubo, Masahiro Kanazaki, Hiroki Nagai

Fifteenth International Conference on Flow Dynamics, Nov, 2019
多目的設計最適化エンジンCHEETAH/Rの開発状況

大山聖

VINAS Users Conference 2019, Oct 10, 2019 Invited
ゼロから始める多目的設計最適化

大山聖

第29回設計工学・システム部門講演会, Sep 25, 2019 Invited
Some Topics on Many Criteria Optimization and Decision Analysis

Akira Oyama

Workshop on Many Criteria Optimization and Decision Analysis, Sep 16, 2019 Invited
Monte-Carlo Evaluation of Control Law for High-Altitude Flight Test of Mars Airplane

Koji Fujita, Hiroki Nagai, Akira Oyama

31st Congress of the International Council of the Aeronautical Sciences, Sep, 2019
Proposal of Benchmark Problem Based on Real-World Car Structure Design Optimization

Takehisa Kohira, Hiromasa Kemmotsu, Akira Oyama, Tomoaki Tatsukawa

The Genetic and Evolutionary Computation Conference 2018, Jul, 2019
Benchmarking Constrained Surrogate-based Optimization on Low Speed Airfoil Design Problems

Pramudita Satria palar, Yohanes Bimo Dwianto, Rommel Regis, Akira Oyama, Lavi Rizki Zuhal

GECCO 2019, Jul, 2019
Ensemble-Based Constraint handling in Multiobjective Optimization

Aljosa Vodopija, Akira Oyama, Bogdan Filipic

GECCO 2019, Jul, 2019
Improved Binary Additive Epsilon Indicator for Obtaining Uniformly Distributed Solutions in Multi-objective Optimization

Tatsumasa Ishikawa, Hiroaki Fukumoto, Akira Oyama, Hiroyuki Nishida

GECCO 2019, Jul, 2019
On Improving the Constraint-Handling Performance with Modified Multiple Constraint Ranking (MCR-mod) for Engineering Design Optimization Problems Solved by Evolutionary Algorithms

Yohanes Bimo Dwianto, Hiroaki Fukumoto, Akira Oyama

GECCO 2019, Jul, 2019
Coverage Enhancement of MOEA-D-M2M for Problems with Difficult-to-Approximate Pareto Front Boundaries

Hiroaki Fukumoto, Akira Oyama

IEEE Congress on Evolutionary Computation 2019, Jun, 2019
Efficient Infill Criterion of Surrogate Model for Severely-Constrained Optimization Problems

Yohanes Dwianto, Hiroki Fukumoto, Akira Oyama

AIAA Aviation Forum 2019, Jun, 2019
An Intrusive Multi-Element Polynomial Chaos Method Based on Edge Detection Technique for Uncertainty Quantification

Shigetaka Kawai, Akira Oyama

3rd International Conference on Uncertainty Quantification in Computational Sciences and Engineering, Jun, 2019
Experimental Investigation of Reynolds Number Effect on the Aeroacoustics Field of a Supersonic Jet

Yuta Ozawa, Taku Nonomura, Akira Oyama, Makoto Yamamoto

25th AIAA/CEAS Aeroacoustics Conference, May, 2019
多目的設計探査ソフトウェアCHEETAH

大山聖

VINASトップソリューション春セミナー２０１９, Apr 19, 2019 Invited
Design, development and stiffness test of mars airplane's wing

Apr 18, 2019
なぜ多数目的最適化アルゴリズムCHEETAHが高速なのか

大山聖

最適設計の計算高速化・コスト削減・設計利用促進オンラインセミナー, Mar 11, 2019 Invited
Preliminary Spacecraft Design Optimization Using Multi-Objective Evolutionary Algorithm

Hiroaki Fukumoto, Mitsuhisa Baba, Masatsugu Otsuki, Yasuhiro Kawakatsu, Akira Oyama

10th International Conference on Evolutionary Multi-Criterion Optimization, Mar, 2019
Study on Multi-objective Design Optimization Of Air Breathing Engine Fan for sounding rocket

斉藤巧真, 大山聖, 小林弘明, 丸祐介

日本機械学会設計工学・システム部門講演会論文集(CD-ROM), 2019, The Japan Society of Mechanical Engineers

Multiobjective design optimization of the engine of the atmosphere-assisted reusable sounding rocket is performed for maximizing the maximum altitude and the payload weight. The result shows that a trade-off between maximization of maximum altitude and payload weight maximization.
Evaluation of Inflow Turbulent Fluctuation Effects on Laminar Seperation Bubbles Using Large Eddy Simulations

Shigetaka Kawai, Kengo Asada, Akira Oyama

AIAA SCITECH FORUM 2019, Jan, 2019
Comparison of Time-Averaged Supersonic Jet Profile Acquired by Particle Image Velocimetry and Shadowgraph Velocimetry Using Single Pixel Ensemble Correlation

Taku Nonomura, Hiroaki Nakano, Yuta Ozawa, Daiki Terakado, Makoto Yamamoto, Kozo Fujii, Akira Oyama

Jan, 2019
Effect of External Rib Structure on Aerodynamic Performance of Thin Wing in Low Reynolds Number

Shun Tamura, Akira Oyama

AIAA SCITECH FORUM 2019, Jan, 2019
Aerodynamic Challenge for Realization of Mars Airplane

NAGAI Hiroki, OYAMA Akira, ANYOJI Masayuki, OKAMOTO Masato, FUJITA Koji, YONEMOTO Koichi

Aeronautical and Space Sciences Japan, 2019, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
Preliminary Conceptual Design of Mars Airplane for RSL Observation

藤田昂志, 永井大樹, 大山聖, 藤田和央

宇宙科学技術連合講演会講演集(CD-ROM), 2019
高速流体力学に関する学術研究

佐藤英一, 大山聖, 福本浩章, 渡邉誉良, 河合成孝, 関本諭志, 田村駿, 寺門大毅, 下村怜, 野々村拓, 石川達将, 江光希, 谷口翔太, 中神貴裕

宇宙航空研究開発機構特別資料 JAXA-SP-(Web), 2019
高速流体力学に関する学術研究

佐藤英一, 大山聖, 李東輝, 福本浩章, 原田拓弥, 中野宏章, 渡邉誉良, 井上翔太, 青木理紗子, 河合成孝, 関本諭志, 田村駿, スラナートスリカンス, 寺門大毅, 小澤雄太, 下村怜, 野々村拓

宇宙航空研究開発機構特別資料 JAXA-SP-(Web), 2019
Application of Deep Reinforcement Learning to Flow Separation Control over Airfoil Utilizing Active Flow Control Device

西田浩之, 下村怜, 関本諭志, 大山聖, 藤井孝蔵

ながれ, 2019
Aerodynamic characteristics of a rotor in low Reynolds number region for Mars Helicopter

江光希, 青木理紗子, 関本諭志, 大山聖

流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム講演集(CD-ROM), 2019
Experimental Study on Closed-loop Flow Separation Control Utilizing Deep Reinforcement Learning on NACA0015 airfoil

下村怜, 関本諭志, 大山聖, 藤井孝藏, 西田浩之

流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム講演集(CD-ROM), 2019
火星航空機翼構造の開発

水上諒, 大山聖, 竹内伸介, 高野敦, Mizukami Ryo, Oyama Akira, Takeuchi Shunsuke, Takano Atsushi

第34回宇宙構造・材料シンポジウム：講演集録 = Proceedings of 34th Symposium on Aerospace Structure and Materials, Dec, 2018, 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)

第34回宇宙構造・材料シンポジウム（2018年12月4日. 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS)), 相模原市, 神奈川県資料番号: SA6000137024レポート番号: B02
Study on Improving Efficiency of Multi-Objective Evolutionary Algorithm with Large Population by M2M Decomposition and Elitist Mate Selection Scheme

Hiroaki Fukumoto, Akira Oyama

2018 IEEE Symposium Series on Computational Intelligence, Nov, 2018
MABE2: 第２回火星飛行機高高度飛行試験

大山聖, 永井大樹, 藤田昂志, 安養寺正之, 岡本正人, 江光希, 金崎雅博, 高野敦, 水上諒, 竹内伸介, 安部明雄, 佐々修一, 布田翼, 満武勝嗣, 得竹浩, 火星探査航空機リサーチグループ, Oyama Akira, Nagai Hiroki, Fujita Koji, Anyoji Masayuki, Okamoto Masato, Koh Mitsuki, Kanazaki Masahiro, Takano Atsushi, Mizukami Ryo, Takeuchi Shinsuke, Abe Akio, Sasa Shuichi, Futa Tsubasa, Mitsutake Katsushi, Tokutake Hiroshi

大気球シンポジウム: 平成30年度 = Balloon Symposium: 2018, Nov, 2018, 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)

大気球シンポジウム平成30年度（2018年11月1-2日. 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS)）, 相模原市, 神奈川県著者人数: 15名ほか資料番号: SA6000128031レポート番号: isas18-sbs-031
Study on Reducing Turn-Around Time of Multi-Objective Evolutionary Algorithm on an Industrial Problem

Hiroaki Fukumoto, Akira Oyama

International Conference on High-Performance Optimization in Industry, Oct, 2018
Stability of split-form flux-reconstruction schemes for airfoil flow simulation with high-order mesh

Takara Watanabe, Yoshiaki Abe, Takanori Haga, Ryoji Takaki, Akira Oyama, Taku Nonomura, Koji Miyaji

tenth international conference on computational fluid dynamics, Jul, 2018
Uncertainty quantification and global sensitivity analysis of airfoil characteristics at low Reynolds numbers

Shigetaka Kawai, Akira Oyama

tenth international conference on computational fluid dynamics, Jul, 2018
High-fidelity compressor blade design optimization using evolutionary algorithm

Akira Oyama, Yongsheng Lian

tenth international conference on computational fluid dynamics, Jul, 2018
Benchmarking Multiobjective Evolutionary Algorithms and Constraint Handling Techniques on a Real-World Car Structure Design Optimization Benchmark Problem

Hiroaki Fukumoto, Akira Oyama

The Genetic and Evolutionary Computation Conference 2018, Jul, 2018
Preliminary Experimental Study on Closed-loop Flow Separation Control Utilizing Deep Q-Network over Fixed Angle-of-Attack Airfoil

Satoshi Shimomura, Satoshi Sekimoto, Hiroaki Fukumoto, Akira Oyama

AIAA Flow Control Conference, Jun, 2018
Experimental analysis of burst actuation for separation control around a pitching NACA0015 airfoil using a DBD plasma actuator at low reynolds number

Satoshi Sekimoto, Hiroaki Fukumoto, Satoshi Shimomura, Kozo Fujii, Akira Oyama, Hiroyuki Nishida

AIAA Aerospace Sciences Meeting, 2018, 2018, American Institute of Aeronautics and Astronautics Inc, AIAA
Aerodynamic design of airfoil for flying wing mars airplane

Takuya Harada, Koji Fujita, Akira Oyama, Hiroya Mamori, Makoto Yamamoto

AIAA Aerospace Sciences Meeting, 2018, 2018, American Institute of Aeronautics and Astronautics Inc, AIAA
A Generic Framework for Incorporating Constraint Handling Techniques into Multi-Objective Evolutionary Algorithms

Hiroaki Fukumoto, Akira Oyama

Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics), 2018, Springer Verlag
Quantitative Evaluation of Effect of Jet Temperature on Acoustic Waves from Supersonic Jets at Mach 2.0 by Large Eddy Simulations

H.Nakano, T.Nonomura, A.Oyama, H.Mamori, N.Fukushima, M.Yamamoto

Proceedings of 2018 AIAA Science and Technology Forum, Jan, 2018
分割型移流項を用いた高次精度流束再構築法の実用計算における安定性について

渡邉誉良, 阿部圭晃, 芳賀臣紀, 高木亮治, 大山聖, 野々村拓, 宮路幸二

数値流体力学シンポジウム講演論文集(CD-ROM), 2018
Conceptual helicopter design for exploration of pit craters and caves on mars

Risako Aoki, Akira Oyama, Koji Fujita, Hiroki Nagai, Kensuke Kanou, Nao Inoue, Shu Sokabe, Masahiro Kanazaki, Kai Tomisawa, Kazufumi Uwatoko

2018 AIAA SPACE and Astronautics Forum and Exposition, 2018
Mars Exploration by Mars Airplane

永井大樹, 大山聖

宇宙科学技術連合講演会講演集(CD-ROM), 2018
Large-eddy simulations of flow control effects of a DBD plasma actuator at various burst frequencies on a dynamic flowfield around a pitching NACA0012 airfoil at reynolds number of 256,000

Hiroaki Fukumoto, Hikaru Aono, Taku Nonomura, Akira Oyama, Kozo Fujii

AIAA Aerospace Sciences Meeting, 2018, 2018
Investigation of maximum velocity induced by body-force fields for simpler modeling of plasma actuators

Shigetaka Kawai, Thijs Bouwhuis, Yoshiaki Abe, Aiko Yakeno, Taku Nonomura, Akira Oyama, Harry W.H. Hoeijmakers, Kozo Fujii

AIAA Aerospace Sciences Forum, Jan, 2018
深層強化学習を用いた固定翼周りの流れに対するフィードバック剥離制御の実験的研究

下村怜, 関本諭志, 福本浩章, 大山聖, 藤井孝蔵, 西田浩之

日本機械学会年次大会講演論文集(CD-ROM), 2018

Professional Memberships

Research Projects

多目的設計探査の導入による風洞試験方法の革新

科学研究費補助金, 日本学術振興会, Apr, 2014 - Mar, 2017

大山聖
世界初の火星飛行探査実現に向けた基盤研究と高高度飛行試験

科学研究費補助金, 日本学術会議, Apr, 2012 - Mar, 2015

永井大樹
固有直交分解を用いたパレート最適解群からの設計知識抽出法の確立と実証

科学研究費補助金, 日本学術振興会, Apr, 2011 - Mar, 2013

大山聖
局在流れに着目したプラズマアクチュエータ流れ制御に関する研究

科学研究費補助金, 日本学術会議, Apr, 2008 - Mar, 2011

藤井孝藏
多目的最適化とデータマイニング手法を用いたはばたき型MAVに関する研究

科学研究費補助金, 日本学術振興会, Apr, 2008 - Mar, 2010

大山聖

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