Curriculum Vitaes

Satoshi Hanaki

  (花木 聡)

Profile Information

Affiliation
Graduate School, of Engineering, University of Hyogo
Degree
(BLANK)(Osaka University)

J-GLOBAL ID
200901003113099833
researchmap Member ID
1000244738

Research Interests

 2

Research History

 1

Misc.

 8
  • 座古勝, 倉敷哲生, 花木聡
    材料, 50(3) 278-283, 2001  
  • 座古 勝, 倉敷 哲生, 花木 聡
    材料, 50(2) 158-162, 2001  
  • M. Zako, T. Kurashiki, S. Hanaki
    Zairyo/Journal of the Society of Materials Science, Japan, 50(3) 278-283, 2001  
  • M. Zako, T. Kurashiki, S. Hanaki
    Zairyo/Journal of the Society of Materials Science, Japan, 50(2) 158-162, 2001  
  • 座古 勝, 高野 直樹, 花木 聡
    材料, 47(1) 90-94, 1998  
  • Masaru Zako, Naoki Takano, Satoshi Hanaki
    Zairyo/Journal of the Society of Materials Science, Japan, 47(1) 90-94, 1998  
  • ZAKO Masaru, TAKANO Naoki, ICHIKAWA Masahiro, HANAKI Satoshi
    Transactions of the Japan Society of Mechanical Engineers Series B, 61(589) 1909-1913, 1995  
    The design concept based on reliability is effective for advanced materials, because advanced materials such as fiber-reinforced composites have variable mechanical properties. In addition, as the failure mode in the low cycle fatigue region differs from that in the high cycle fatigue region, it is difficult to predict the fatigue life of advanced materials. So far, we have developed a design margin decision system based on reliability by evaluating fatigue life. In this study, the system is improved for application to advanced materials and a method to divide whole sets of data into the above two regions and to calculate the design margin in each region is presented. From numerical examples for CF/PEEK laminates and epoxy resin, it is revealed that a more reasonable S-N curve and design margin are obtained by the proposed system.
  • Masaru Zako, Naoki Takano, Masahiro Ichikawa, Satoshi Hanaki
    Transactions of the Japan Society of Mechanical Engineers., 61(589) 1909-1913, 1995  
    The design concept based on reliability is effective for advanced materials, because advanced materials such as fiber-reinforced composites have variable mechanical properties. In addition, as the failure mode in the low cycle fatigue region differs from that in the high cycle fatigue region, it is difficult to predict the fatigue life of advanced materials. So far, we have developed a design margin decision system based on reliability by evaluating fatigue life. In this study, the system is improved for application to advanced materials and a method to divide whole sets of data into the above two regions and to calculate the design margin in each region is presented. From numerical examples for CF/PEEK laminates and epoxy resin, it is revealed that a more reasonable S-N curve and design margin are obtained by the proposed system.

Professional Memberships

 2