Tail end structure for an aircraft fuselage

Details Tail end structure for an aircraft fuselage Tail end structure for an aircraft fuselage

1986-07-16

1987-12-15

Barefoot, Galen

Aeronautics and astronautics

Aircraft structure

Fuselage and body construction

B64C 100

Patent

active

047127511

ABSTRACT:
The tail end structure of an aircraft has a cross-sectional configuration th 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.

REFERENCES:
patent: 3023860 (1962-03-01), Ellzey
patent: 3955781 (1976-05-01), Tupolev et al.

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