| タイトル | 人力飛行機用炭素繊維強化プラスチックの強度 |
| その他のタイトル | Strength of CFRP laminates for Human-powered Airplane |
| 著者（日） | 岡部徳之; 中村, 俊一郎 |
| 著者（英） | Iokabe, Toshiyuki; Nakamura, Shunichiro |
| 著者所属（日） | 第一工業大学航空宇宙工学科; 第一工業大学航空工学科 |
| 著者所属（英） | Department of Aerospace Engineering, Daiichi Institute of Technology; Department of Aeronautical Engineering, Daiichi Institute of Technology |
| 発行日 | 2012-03 |
| 発行機関など | 第一工業大学
Daiichi Institute of Technology |
| 刊行物名 | 第一工業大学研究報告
Research Report, Daiichi Institute of Technology |
| 号 | 24 |
| 開始ページ | 21 |
| 終了ページ | 27 |
| 刊行年月日 | 2012-03 |
| 言語 | jpn
eng |
| 抄録 | In the design of the human-powered airplane, the design of beams for wing spar and fuselage are important from the perspective of flight safety. Recently, pipes made with carbon fiber reinforced plastics (CFRPs) are used for the beams. Usually these beams have each CFRP laminate with different lamina-layups according to their individual strength requirement. In this report, three types of laminates were tested to obtain their tensile and bearing strength. As a result of this study, each laminate has different strength according to the layups. |
| 内容記述 | 形態: カラー図版あり
Physical characteristics: Original contains color illustrations |
| キーワード | human-powered airplane; laminate layup; tensile and bearing strengths |
| 資料種別 | Departmental Bulletin Paper |
| ISSN | 2187-0462 |
| NCID | AN10303695 |
| SHI-NO | AA0065422004 |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/14744 |
