| タイトル | 人力飛行機の外翼の空力設計検討 |
| その他のタイトル | The Wing Design for the Outer Wing Area of the Man Powered Airplane |
| 著者（日） | 酒井, 謙二 |
| 著者（英） | Sakai, Kenji |
| 著者所属（日） | 第一工業大学 |
| 著者所属（英） | Daiichi Institute of Technology |
| 発行日 | 2013-03 |
| 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 |
| 号 | 25 |
| 開始ページ | 1 |
| 終了ページ | 5 |
| 刊行年月日 | 2013-03 |
| 言語 | jpn
eng |
| 抄録 | The man powered airplane's wing geometry was designed in order to reduce the pitching moment for outer wing area. The DAE21 wing geometry is used for many man powered airplanes. But when this wing geometry is used for all span area, the nose down pitching moment is calculated for the wing outer area. New wing geometry is designed, named DAE30, which has the maximum chamber line's position is 30% wing section. By using this wing geometry, the nose down pitching moment has been deduced for the design speed. |
| 内容記述 | 形態: カラー図版あり
Physical characteristics: Original contains color illustrations |
| キーワード | Man Powered Airplane; Wing Geometry; Pitching Moment; Outer Wing Area |
| 資料種別 | Research Paper |
| NASA分類 | Aerodynamics |
| ISSN | 2187-0462 |
| NCID | AN10303695 |
| SHI-NO | AA0062349001 |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/21990 |
