HISAKI Project Team

中村 俊哉

ナカムラ トシヤ  (Toshiya Nakamura)

基本情報

所属
国立研究開発法人宇宙航空研究開発機構 宇宙科学研究所 宇宙飛翔工学研究系 特任教授
学位
工学博士(1991年3月 東京大学)

研究者番号
60237419
ORCID ID
 https://orcid.org/0000-0002-2403-5780
J-GLOBAL ID
202101015987830507
researchmap会員ID
R000025142

論文

 56
  • Toshiya Nakamura
    Mathematics in Engineering, Science and Aerospace 17(1) 87-99 2026年3月  査読有り筆頭著者責任著者
    This study investigated the characteristics of the amorphous material fatigue model proposed by Kurotani et al. concerning the rate/time-dependent material instability and the fatigue damage initiation process. Stress relaxation simulations showed that, in this model, two mechanisms compete, one of which increases the density fluctuations by mechanical deformation and the other decreases them over time. In fatigue simulations, the density fluctuation gradually becomes nonuniform, resulting in damage generation. During this process, the density fluctuations form a band-like pattern in the principal-stress direction, and the equivalent strain forms a pattern along the shear direction. We demonstrated that the model could provide mesoscopic insights into the mechanical properties of amorphous materials.
  • Toshiya Nakamura
    Mathematics in Engineering, Science and Aerospace 15(3) 889-901 2024年9月  査読有り筆頭著者責任著者
    The interfacial stress between fibers and matrix plays an important role in the durability and damage initiation of carbon fiber reinforced composites. In this study, thermoelastic analysis was performed on a plate containing randomly distributed multiple fibers. Complex stress functions were employed with a semi-numerical method to ensure displacement continuity along the fiber/matrix interface as a boundary condition. The statistical investigation reveals that the stress concentration due to the presence of multiple fibers increases as the fiber density increases, though its deviation decreases. A numerical case study was conducted to discuss the micromechanics of the inherent scatter of material strength. The stress-strength model with Monte-Carlo simulation demonstrated the fracture probability calculation. The uncertainty obtained is partially attributed to the micromechanical stress variation around the fibers.
  • Hiroki Kawabe, Yuichiro Aoki, Toshiya Nakamura
    AIAA Journal 62(4) 1311-1317 2024年4月  査読有り
    The objective of this study is to develop a novel aircraft design approach using biomimetics as an alternative to traditional airframes. This approach is primarily inspired by the dragonfly wing, which possesses reinforcement structures composed of cross veins and longitudinal veins. These structures are assumed to regulate deformation and enhance stiffness, respectively. The cross veins were replicated using weighted centroidal Voronoi tessellation (WCVT) based on the out-of-plane displacement of the skin. In contrast, the longitudinal veins were replicated by extracting a centerline from the topology optimization (TO) results on the skin, achieved through image analysis techniques such as binarization and skeletonization. The longitudinal layout effectively reduces compliance by distributing internal loads, utilizing only essential reinforcements on the skin without increasing its mass. The WCVT layout significantly enhances the buckling resistance of the reinforced skin. As a result, the skin reinforced using both cross–longitudinal layouts from TO and WCVT exhibited a buckling load 2.7 times greater while maintaining a lower mass compared to conventional layouts.
  • Hiroshi Suemasu, Yuichiro Aoki, Hikaru Hoshi, Yasutomo Tateishi, Sunao Sugimoto, Toshiya Nakamura
    Composites Part A: Applied Science and Manufacturing 172 2023年9月  査読有り
  • Hiroshi Suemasu, Yuichiro Aoki, Yasutomo Tateishi, Sunao Sugimoto, Toshiya Nakamura
    Journal of Composite Materials 57(21) 3377-3391 2023年9月  査読有り

MISC

 28

講演・口頭発表等

 190

所属学協会

 3

共同研究・競争的資金等の研究課題

 3