Researcher Profile and Settings

Affiliation

• Faculty of Engineering　Mechanical and Aerospace Engineering　Mechanics and Materials

Job Title

• Associate Professor

Degree

• Ph. D. in Engineering（2009/03 Hokkaido University）

J-Global ID

• 201201085824423198

Research Interests

• 最適設計   スマート構造   圧電素子   曲線状繊維   振動モード   繊維強化複合材料   打撃試験   周波数応答関数   振動試験   

Research Areas

• Manufacturing technology (mechanical, electrical/electronic, chemical engineering) / Control and systems engineering
• Manufacturing technology (mechanical, electrical/electronic, chemical engineering) / Design engineering
• Informatics / Mechanics and mechatronics
• Manufacturing technology (mechanical, electrical/electronic, chemical engineering) / Machine materials and mechanics

Educational Organization

•  Bachelor's degree program　School of Engineering
•  Master's degree program　Graduate School of Engineering
•  Doctoral (PhD) degree program　Graduate School of Engineering

Academic & Professional Experience

• 2013/11 - Today 北海道大学 工学(系)研究科(研究院) 准教授
• 2013/09 - 2014/06 ETH Zurich
• 2009/04 - 2013/10 北海道大学 工学(系)研究科(研究院) 助教
• 2007/04 - 2009/03 Hokkaido Univ.

Education

• 2007/04 - 2009/03  Hokkaido University  Graduate School of Engineering

Research Activities

Published Papers

• Manufacturability and Deformation Performances of CFRP Twist Morphing Wing Structure with Applying the Electrodeposition Resin Molding Method

  Kazuaki Katagiri, Daekwi Kim, Choong Sik Park, Sonomi Kawakita, Masato Tamayama, Koki Kayano, Shinya Honda, Katsuhiko Sasaki, Makoto Yamazaki

  PROCEEDINGS OF THE 2021 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY (APISAT 2021), VOL 1 912 879 - 891 1876-1100 2023 

  To achieve efficient flight by minimizing energy consumption, a morphing wing that allows large and smooth deformation similar to a wing of a migratory bird is required. Previously, the authors have developed a migratory-sized unmanned aerial vehicle (UAV) with a twist morphing wing. The twist morphing wing was manufactured using a carbon fiber reinforced plastics (CFRP) with applying the electrodeposition resin molding (ERM) method, which was developed by authors. In the ERM method, resin impregnation proceeds in a liquid by electrophoresis. Thus, manufacturing process is very efficient because neither pressurization nor evacuation are necessary. On the other hand, although the molding of the twist morphing wing is efficient, an optimal design is important for the twist morphing wing to lower the torsional rigidity to reduce the driving force of the morphing and increase the bending rigidity to support aerodynamic loads. Therefore, in this study, the spar of the twist morphing wing was designed to be arranged in a triangle. Furthermore, the twist morphing wing structures were fabricated by the ERM method, and by a 3D printer for benchmarking. So, torsion and bending deformation properties of the twist morphing wing were confirmed under the aerodynamic loading condition, and validated by finite element analysis. As a result, it was confirmed that the manufacturing efficiency of the ERM method was superior to that of the 3D printer. Additionally, the torsional rigidity of the twisted morphing wing was almost the same, regardless of the manufacturing method. Furthermore, the bending rigidity of the specimen manufactured by the ERM method was higher than that of the 3D printer.
• Impact properties of carbon fiber/cellulose nanofiber reinforced epoxy composite using asymmetric stacking sequence of non-hydrophobic cellulose nanofiber dispersion layer

  Kazuaki Katagiri, Naoko Kishimoto, Haruna Yamaguchi, Toshihiko Okumura, Sonomi Kawakita, Shinya Honda, Katsuhiko Sasaki

  MECHANICS OF ADVANCED MATERIALS AND STRUCTURES 1537-6494 2022/06 

  Cellulose nanofibers (CNFs) are sustainable materials with high specific strengths. To enhance the impact properties of carbon fiber reinforced plastics (CFRPs), the authors have developed an efficient process for incorporating a non-hydrophobized CNF dispersion layer into CFRPs. In this study, the impact properties of CFRP with asymmetrically stacked CNF dispersion layer was investigated by conducting the instrumented Charpy impact tests. Two types of CNFs were used for comparison. Consequently, by inserting the CNF dispersion layer into the opposite side of the striking surface, the Charpy impact value increased by 26% compared to CFRP without CNF dispersion layer.
• Vibration optimization of laminated composites with curvilinear reinforcing fibers for shell structures

  SAIWAKI Isamu, HONDA Shinya, KATAGIRI Kazuaki, SASAKI Katsuhiko, TAKEDA Ryo

  The Proceedings of the Dynamics & Design Conference 一般社団法人 日本機械学会 2022 145  2022 

  Tailored Fiber Placement (TFP) is an embroidery technique that enables it possible to design free fiber shapes on base material sheets. The TFP generally creates curved fibers on a flat surface. However, CFRP structures are often used as shell structures rather than as flat plates, and there is not enough research to design fiber shapes on curved surfaces. In this research, we applied our previous optimization method for curved fiber shapes to shell structures. Curved fiber shapes were created by the linear combination of radial basis functions (RBFs) to represent complex fiber shapes. The fiber shape on a curved surface was represented by projecting the fiber shape on a plane surface using a coordinate transformation technique. Using this method, we investigated optimum fiber shapes to improve the first natural frequency of shell structure composites. The results showed that the optimum fiber shape gave higher natural frequencies than the linear fiber orientation. Obtained optimum fiber shape resulted in higher natural frequencies than the linear fiber orientation.
• Damping identification and optimization of laminated composites with curved reinforcing fibers

  Honda Shinya, Takisawa Hiraku, Katagiri Kazuaki, Sasaki Katsuhiko, Takeda Ryo

  NCTAM papers, National Congress of Theoretical and Applied Mechanics, Japan 日本学術会議 「機械工学委員会・土木工学・建築学委員会合同IUTAM分科会」 66 163  2022 

  The effect of both curvilinear fiber orientation and the resulting thickness distribution on modal damping of carbon fiber reinforced plastics (CFRP) fabricated by electrodeposition resin molding (ERM) was investigated in this study. Tailored fiber placement (TFP) is employed to manufacture carbon fiber preforms with continuous curvilinear fiber paths. Damping of CFRP fabricated by ERM was calculated using the concept of specific damping capacity (SDC). Optimization of fiber shapes in L-shaped plate model was conducted to maximize the first modal SDC using particle swarm optimization (PSO). As a result, the optimum fiber shape successfully improves both the first natural frequency and modal SDC in comparison with several unidirectional fiber shapes.
• Optimum design of curvilinear reinforcing fiber shapes for CFRP plates fabricated by electrodeposition resin molding method

  HONDA Shinya, TAKISAWA Hiraku, KATAGIRI Kazuaki, SASAKI Katsuhiko, TAKEDA Ryo

  The Proceedings of OPTIS 一般社団法人 日本機械学会 2022.14 U00010  2022 

  Fiber shape optimization was performed to improve the damping properties of CFRP fabricated by electrodeposition resin molding (EDRM) method. Damping properties of composites were modeled by the specific damping capacity (SDC), and the material damping parameters required for numerical estimation were identified by an inverse analysis using results of experimental modal analysis and finite element analysis. In the optimization, a curvilinear fiber shape that maximizes the first mode SDC was explored. The thickness distribution due to the curvilinear fiber shape was estimated and applied to the finite element analysis. The fiber shapes obtained by the optimization improved the first natural frequencies and mode SDCs compared to several straight fiber orientations, indicating that the curved fiber orientation is effective in improving damping.

Books etc

• CFRP/CFRTPの界面制御、成形加工技術と部材応用

  技術情報協会 (Contributor第5節 刺繍機と電着樹脂含浸法を用いた成形技術)
  技術情報協会 2020/12 (ISBN: 9784861048111) 586p

MISC

• Strength of CFRP I-shaped beam with cellulose nanofibers dispersed on the surface

  片桐一彰, 山口真平, 永廣卓哉, 園村浩介, 尾崎友厚, 川北園美, 武村守, 吉岡弥生, 本田真也, 佐々木克彦, 南沙也加, 金大貴  日本複合材料合同会議(Web)  9th-  2018
• Mechanical properties of CFRP corrugation manufactured by electro-activated deposition molding

  片桐一彰, 山口真平, 永廣卓哉, 川北園美, 武村守, 吉岡弥生, 佐々木克彦, 本田真也, 南沙也加, LIGINE Florian  飛行機シンポジウム講演集(CD-ROM)  56th-  2018
• 電着を用いた樹脂含浸法を適用したCFRPの強度特性

  片桐一彰, 佐々木克彦, 本田真也, 冨沢祐介, 中島晶, 南沙也加, 山口真平, 尾崎友厚, 園村浩介, 垣辻篤  構造強度に関する講演会講演集  59th-  2017
• Addition of Heat Storage Properties to CFRP by Using Electoro-activated Resin Molding

  片桐一彰, 山口真平, 永廣卓哉, 尾崎友厚, 園村浩介, 吉岡弥生, 垣辻篤, 後藤凌平, 戸谷剛, 南沙也加, 本田真也, 佐々木克彦  宇宙科学技術連合講演会講演集(CD-ROM)  61st-  2017
• Molding and strength of CFRP by using electro-activated deposition

  片桐一彰, 山口真平, 永廣卓哉, 尾崎友厚, 園村浩介, 吉岡弥生, 垣辻篤, 南沙也加, 本田真也, 佐々木克彦  飛行機シンポジウム講演集(CD-ROM)  55th-  2017
• 302 Optimization of the smart laminated composites for the vibration control

  HONDA Shinya, NARITA Yoshihiro, KAJIWARA Itsuro, NAKAMURA Satoshi  最適化シンポジウム講演論文集  2010-  (9)  "302  -1"-"302-5"  2010/12/09  

  The present smart composite structures are composed of PZT actuators and graphlte-epoxy composites to improve the performance of vibration suppression. The control performance of PZT actuators strongly depends on their placements and vibration characteristics of laminated composites are varied by their lay-up configurations. Thus, a multidisciplinary optimization method employing actuator placements, lay-ups of laminated composite plates and control systems as design variables is proposed here. First, a database containing the frequencies and modal matrixes is made to avoid the FEA repeatedly. Then, the H_2 norm of control response is minimized with respect to the above design variables with referring the database by a simple genetic algorithm with assuming that the state feedback is available. Finally, the output feedback system is reconstructed with the dynamic compensator based on the linear matrix inequality (LMI) approach. The effectiveness of the present optimization technique is confirmed by the experimental and numerical results.
• 105 Numerical Simulation and Experiment for the Multilink System

  Kitagawa Yu, Maeda Hideki, Narita Yoshihiro, Honda Shinya  北海道支部講演会講演概要集  2010-  (49)  9  -10  2010/11/07
• 103 Vibration Analysis for the Link System of Rigid and Elastic Bodies with Elastic Hinges

  Maeda Hideki, Kitagawa Yu, Honda Shinya, Narita Yoshihiro  北海道支部講演会講演概要集  2010-  (49)  5  -6  2010/11/07
• 102 Vibration Analysis of laminated Spherical Shells with Fixed Two Poles

  FUJII Toshinori, HONDA Shinya, NARITA Yoshihiro  北海道支部講演会講演概要集  2010-  (49)  3  -4  2010/11/07
• 207 Vibration Property of Laminated VGCF/Al Circular Plates

  KOYA Naoaki, HONDA Shinya, NARITA Yoshihiro  北海道支部講演会講演概要集  2010-  (49)  33  -34  2010/11/07
• 209 Stacking sequence optimization of a laminated elliptical plate

  Lee Seung-Cheol, HONDA Shinya, NARITA Yoshihiro  北海道支部講演会講演概要集  2010-  (49)  37  -38  2010/11/07
• 108 Stacking sequence optimization of rotating rectangular plate under centrifugal force

  WADA Masaaki, HONDA Shinya, NARITA Yoshihiro  北海道支部講演会講演概要集  2010-  (49)  15  -16  2010/11/07
• 213 Vibration optimization for composite model plate reinforced by practical curvilinear fiber

  Yugami Kumpei, Honda Shinya, Narita Yoshihiro  北海道支部講演会講演概要集  2010-  (49)  45  -46  2010/11/07
• 109 Vibrational optimization for locally reinforced CFRP/Al Hybrid Plates

  KOSHIBA Takashi, HONDA Shinya, NARITA Yoshihiro  北海道支部講演会講演概要集  2010-  (49)  17  -18  2010/11/07
• 214 Vibration characteristics of circular pipes with filling materials

  MINAMI Takashi, HONDA Shinya, NARITA Yoshihiro  北海道支部講演会講演概要集  2010-  (49)  47  -48  2010/11/07
• 3203 Kansei Evaluation for Perception of Objects : Focus on the Relationship between 3D object model and impression

  LEE Miyong, HONDA Shinya, NARITA Yoshihiro  設計工学・システム部門講演会講演論文集  2010-  (20)  "3203  -1"-"3203-2"  2010/10/27  

  It is different by an individual how to feel about objects, and it is a subjective characteristic by the Kansei of the individual. This study aimed to evaluate an impression of the three-dimensional objects using the Kansei evaluation, and to investigate an element of the 3D objects and the connection with the impression. As the results of experiment, the shapes which became the first impression correspond with the element of the 3D objects. Therefore we think that the elements and the impressions are related deeply. This study becomes the fundamental researches in the manufacturing such as mechanical engineering, Kansei engineering and the product design.
• 2401 User Category based on Quantitative Information in Kansei Evaluation

  LEE Miyong, HONDA Shinya, NARITA Yoshihiro  The Computational Mechanics Conference  2010-  (23)  485  -486  2010/09/23
• 1501 Multidisciplinary design optimization of smart composites for vibration control

  HONDA Shinya, NARITA Yoshihiro, KAJIWARA Itsuro  The Computational Mechanics Conference  2010-  (23)  580  -581  2010/09/23
• 134 Simultaneous Optimization of Surface Shapes and Lay-up Configurations for Composite Shells

  Kato Takeru, HONDA Shinya, NARITA Yoshihiro  Dynamics & Design Conference  2010-  "134  -1"-"134-6"  2010/09/14  

  Shapes and lay-up configurations of composite laminated shallow shells are optimized simultaneously to maximize the fundamental frequency by a simple genetic algorithm method with the elitist tactics. The shell shape is defined by a cubic polynomial and various shapes of shells with inconstant curvature radii can be expressed by varying the value of coefficient for each term. The coefficients and the lay-up configuration of the laminated shell are directly employed as design variables, and constraints are imposed on the coefficients and curvature radii to keep shells shallow. The frequencies are calculated by using the Ritz method due to its flexibleness for shell shapes. Results of the present analysis technique agreed well with experimental and finite element analysis results in terms of frequencies and mode shapes, obtained optimum solutions resulted in higher fundamental frequencies than the shells with general shapes and lay-up configurations.
• 133 Experimental Modal Analysis and Optimization of Composite Material Model Reinforced by Curvilinear Fibers

  HONDA Shinya, YUGAMI Kumpei, NARITA Yoshihiro  Dynamics & Design Conference  2010-  "133  -1"-"133-5"  2010/09/14  

  The vibration characteristics of the composite plate model with curvilinear fibers are investigated in this study. The curvilinear fiber is realized by the plastic deformation of steel wires and the present composite model is composed of the curved steel wires and epoxy resin. The natural frequency and mode shape are obtained by the experimental modal analysis method where the plate is excited by the impulse hammer and acceleration response is measured. The experimental results showed that the present model has the specific skewed mode shape and it agrees well with the finite element analysis result in terms of the frequency and mode shape. Then the curvilinear fiber shape is optimized for the maximum fundamental frequency by using the genetic algorithm method. The numerical results showed that the optimum curvilinear fiber results in the higher fundamental frequency than the plate with typical curvilinear fibers.
• 419 Minimum Design of Stress Concentration for Laminated Composite Plates with Curvilinearly Shaped Fibers

  Owatari Kosuke, Honda Shinya, Narita Yoshihiro  北海道支部講演会講演概要集  2009-  (48)  143  -144  2009/11/28
• 101 Study on Free Vibration of Twisted Thin Panels

  AOKI Ryoji, HONDA Shinya, NARITA Yoshihiro  北海道支部講演会講演概要集  2009-  (48)  1  -2  2009/11/28
• 105 Analysis of Laminated VGCF/Al Circular Plates Considering Thermal Effects

  KOYA Naoaki, HONDA Shinya, NARITA Yoshihiro  北海道支部講演会講演概要集  2009-  (48)  9  -10  2009/11/28
• 111 Experiment and Dynamic Analysis of Hanging Structural Components : 2^ report. Experimental analysis

  Maeda Hideki, Kitagawa Yu, Narita Yoshihiro, Honda Shinya  北海道支部講演会講演概要集  2009-  (48)  21  -22  2009/11/28
• 102 Vibration Property of Laminated Hybrid Plates

  KOSHIBA Takashi, NARITA Yoshihiro, HONDA Shinya  北海道支部講演会講演概要集  2009-  (48)  3  -4  2009/11/28
• 110 Dynamic Analysis and Experiment of Hanging Structural Components : 1^ report. Theoretical analysis

  Kitagawa Yu, Maeda Hideki, Narita Yoshihiro, Honda Shinya  北海道支部講演会講演概要集  2009-  (48)  19  -20  2009/11/28
• 107 Experimental Verification for Vibration Property of Shallow Shells with Various Curvatures

  Kato Takeru, Narita Daisuke, Honda Shinya, Narita Yoshihiro  北海道支部講演会講演概要集  2009-  (48)  13  -14  2009/11/28
• 106 Optimum Solutions and Experimental Verification for Vibration of Laminated Parallelogram Plates

  FUJII Toshinori, HONDA Shinya, NARITA Yoshihiro  北海道支部講演会講演概要集  2009-  (48)  11  -12  2009/11/28
• 231 Vibration Analysis and Optimization of Laminated Parallelogram Plates Based on the FSDT

  FUJII Toshinori, HONDA Shinya, NARITA Yoshihiro  Dynamics & Design Conference  2009-  "231  -1"-"231-6"  2009/08/03  

  The carbon fiber reinforced plastics (CFRP) is classified as high performance composite materials that are superior to conventional materials in the specific strength and stiffness ratios. They are applied to light-weight structures in aircraft and space industries. In such fields, wings are often approximated as a parallelogram plate, but the past studies were carried out by using the classical plate theory. This analysis is however based on the shear deformation plate theory (FSDT). A Ritz method is used to calculate natural frequencies of symmetrically laminated parallelogram plates, and the layerwise optimization method is used to optimize the best lay-up designs. It is shown that the LO method is applicable to the parallelogram plates successfully.
• 254 Vibration Analysis and Optimization of Laminated Hybrid Thick Plates

  KOSHIBA Takashi, HONDA Shinya, NARITA Yoshihiro  Dynamics & Design Conference  2009-  "254  -1"-"254-6"  2009/08/03  

  A method of analysis is presented for determining the free vibration frequencies of hybrid laminated plates, and the layerwisr optimization method is used to determine the optimum fiber orientation angles for the maximum fundamental frequency under general edge conditions. The hybrid plates made of aluminum core and CFRP skins are made for reducing the material costs. Based on the first-order shear deformation theory (FSDT) applicable to thick plates, the Ritz solution is used to derive a frequency equation, and these results give good agreement with those from finite element method. An extensive set of numerical results is given in tabular and graphical form, illustrating the maximum fundamental frequency with the optimum lay-ups of the laminated hybrid plates. Comparison of the results gives tendencies caused by boundary conditions and laminated composition.
• OS0501 Buckling Analysis for Fiber Reinforced Composite Materials with Local Anisotropy

  HONDA Shinya, OONISHI Yoshimasa, NARITA Yoshihiro  M&M材料力学カンファレンス  2009-  357  -358  2009/07/24
• 208 Maximizing the fundamental frequency of laminated composite plates with optimally shaped curvilinear fibers

  HONDA Shinya, NARITA Yoshihiro, SASAKI Katsuhiko  最適化シンポジウム講演論文集  2008-  (8)  185  -190  2008/11/26  

  A new design method is proposed here to maximize the fundamental frequency of laminated composite plates reinforced by curvilinear fibers. Spline functions represent arbitrarily shaped fibers and Ritz solutions generate frequency equations. The optimum curvilinear shapes are searched for the maximum fundamental frequencies using genetic algorithms, and the increments of data points which define the spline shape are used as design variables under the limited range of undulation. Comparison of the present analysis method gives good agreement with the finite element method in terms of natural frequencies and vibration modes, and the optimized results show that the present plate with optimally shaped curvilinear fibers gives higher or equal fundamental frequencies than those of the conventional plate with optimally oriented parallel fibers.
• 169 Optimization Method for Vibration of Fibrous Composite Plates : Comparison between Experimental Design and Other Methods

  上甲 康之, 趙 希禄, 本田 真也, 成田 吉弘  Dynamics & Design Conference  2008-  "169  -1"-"169-6"  2008/09/02  

  It is desirable to optimize the fiber orientation angles to maximize the fundamental frequencies of the fiber reinforced plastic plates. The optimization is studied here by using the experimental design for nonlinear problems, and it turned out that significantly less number of calculations is necessary as compared to other methods, such as a layerwise optimization approach (LOA). The numerical examples show that assumption of appropriate level values is efficient to obtain the optimum frequency in the vibration problem.
• 406 Locally Anisotropic Design of Fibrous Composite Plate with Optimally Distributed Short Fibers

  HONDA Shinya, NARITA Yoshihiro, SASAKI Katsuhiko  北海道支部講演会講演概要集  2007-  (46)  105  -106  2007/09/29
• 203 Vibration Design of Fibrous Composite Plate with Optimally Distributed Short Fibers

  HONDA Shinya, NARITA Yoshihiro  Dynamics & Design Conference  "203  -1"-"203-6"  2007  

  A new design method of functional fiber reinforced plastics (FRP) materials which imitates the micro structure of bone or shell in the natural world is proposed in this work. The material has local anisotropy induced by optimally distributed short fibers. The present design method combines a genetic algorithm method (GA) with layerwise optimization concept. The first frequency of thin plates is chosen as an objective function to be maximized in the optimization and it is turned out that the present plates always give higher natural frequencies compared to conventional plates which are reinforced by parallel fibers. Moreover, it is also revealed that optimally distributed short fibers tend to be allocated with certain tendency.
• 224 Minimum Weight Design on Buckling of Laminated Plates Using Lamination Parameters

  HONDA Shinya, NARITA Yoshihiro  最適化シンポジウム講演論文集  2006-  (7)  275  -280  2006/12/08  

  A lamination parameter approach, recently proposed by the authors, is extended in this work to solve a minimum weight design problem for optimizing buckling behavior of laminated composite plates. The present approach basically consists of two parts: the first part is to optimize the lamination parameters by a gradient method, and the second part is to obtain the optimum lay-up (i.e., the fiber orientation angles) by minimizing the errors between the optimum parameters and the parameters for all possible discrete lay-up designs. In the extension of approach, the minimum number of layers with equal thickness is determined so that the plate has higher buckling loads than the specified values. Numerical examples demonstrate that the proposed approach is quite effective in determining the optimum lay-ups for the minimum weight design.
• 313 Minimum Weight Design on Buckling of Laminated Plates

  HONDA Shinya, NARITA Yoshihiro, SASAKI Katsuhiko  北海道支部講演会講演概要集  2006-  (45)  105  -106  2006/09/25
• 726 Vibration and Discrete Optimization of Laminated Plates by Using Lamination Parameters

  NARITA Yoshihiro, HONDA Shinya  Dynamics & Design Conference  2005-  "726  -1"-"726-6"  2005/08/22  

  The fiber reinforced plastics (FRP) have been utilized in applications of automobile and aircraft structures, since they have advantages of high specific strength and stiffness ratios. The FRP composites are typically fabricated by stacking orthotropic layers, each composed of reinforcing parallel fibers and matrix material. In this work, the optimum lamination parameters are determined by the mathematical programming, and the corresponding fiber orientation angles are derived by minimizing the error of the optimized parameters and possible sets of discrete fiber orientation angles. Numerical examples show various applications of optimization in vibration behaviors of laminated plates, including the maximum fundamental frequencies with corresponding optimum lay-ups (fiber orientation angles) and the maximum difference of the fundamental and second natural frequencies.

Awards & Honors

• 2017/04 JSME Best Paper Award of JSME
   双安定性を有する複合材シェルのスナップスルー変形に関する多目的最適化 

  受賞者: Shinya HONDA;Keisuke Takahashi;Yoshihiro Narita
• 2015/08 日本機械学会 機械力学計測制御部門 オーディエンス表彰
   双安定性を有する複合材シェルのスナップスルー変形に関する多目的最適化 

  受賞者: 本田真也
• 2011/04 日本機械学会 奨励賞(研究)
   局所的な異方性を有する繊維強化複合材料の解析と最適設計の研究 

  受賞者: 本田真也
• 2011/01 第53回自動制御連合講演会 優秀発表賞
   積層複合材のスマート化による振動制御を目的とした統合最適化 

  受賞者: 本田真也

Educational Activities

Teaching Experience