研究者業績

花木 聡

ハナキ サトシ  (Satoshi Hanaki)

基本情報

所属
兵庫県立大学 大学院 工学研究科 助手
学位
博士(工学)(大阪大学)

J-GLOBAL ID
200901003113099833
researchmap会員ID
1000244738

研究キーワード

 2

経歴

 1

MISC

 8
  • 座古勝, 倉敷哲生, 花木聡
    材料 50(3) 278-283 2001年  
  • 座古 勝, 倉敷 哲生, 花木 聡
    材料 50(2) 158-162 2001年  
  • M. Zako, T. Kurashiki, S. Hanaki
    Zairyo/Journal of the Society of Materials Science, Japan 50(3) 278-283 2001年  
  • M. Zako, T. Kurashiki, S. Hanaki
    Zairyo/Journal of the Society of Materials Science, Japan 50(2) 158-162 2001年  
  • 座古 勝, 高野 直樹, 花木 聡
    材料 47(1) 90-94 1998年  
  • Masaru Zako, Naoki Takano, Satoshi Hanaki
    Zairyo/Journal of the Society of Materials Science, Japan 47(1) 90-94 1998年  
  • 座古 勝, 高野 直樹, 市川 昌弘, 花木 聡
    日本機械学会論文集 61(589) 1909-1913 1995年  
    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.
  • 座古 勝, 高野 直樹, 市川 昌弘, 花木 聡
    日本機械学会論文集. A編 61(589) 1909-1913 1995年  
    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.