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Other TitleThe Wing Design for the Outer Wing Area of the Man Powered Airplane
Author(jpn)酒井, 謙二
Author(eng)Sakai, Kenji
Author Affiliation(jpn)第一工業大学
Author Affiliation(eng)Daiichi Institute of Technology
Issue Date2013-03
Daiichi Institute of Technology
Publication title第一工業大学研究報告
Research Report
Start page1
End page5
Publication date2013-03
AbstractThe 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.
Description形態: カラー図版あり
Physical characteristics: Original contains color illustrations
KeywordsMan Powered Airplane; Wing Geometry; Pitching Moment; Outer Wing Area
Document TypeResearch Paper
NASA Subject CategoryAerodynamics

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