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Title:
DEFORMED FUSELAGE AND TAIL SECTION OF AIRCRAFT
Document Type and Number:
Japanese Patent JPS6226200
Kind Code:
A
Abstract:
The tail end structure of an aircraft has a cross-sectional configuration with laterally and downwardly extending lobes reaching outside a circular cross-section tail end structure, yet staying within the silhouette of the circular cross-section tail end structure as viewed from the top, the side, and the bottom, whereby the boundary layer formation and the boundary layer separation are improved as compared to a tail end structure having the circular cross-section.

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Inventors:
ERUNSUTO HAINRITSUHI HIRUSHIER
Application Number:
JP17292486A
Publication Date:
February 04, 1987
Filing Date:
July 24, 1986
Export Citation:
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Assignee:
MESSERSCHMITT BOELKOW BLOHM
International Classes:
B64C7/00; B64C1/00; B64C23/00; (IPC1-7): B64C7/00; B64C23/00
Attorney, Agent or Firm:
Ezaki Mitsuyoshi



 
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