Supersonic aircraft with the engines disposed under the delta wi

Aeronautics and astronautics – Aircraft – heavier-than-air – Airplane sustained

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244119, B64C 100

Patent

active

039557812

ABSTRACT:
A supersonic aircraft in which the engines are disposed under the middle portion of a delta wing and the contour of the nose portion except for the front end of the fuselage is defined essentially by two arcs of different circumference, the circumferences being disposed one above the other, with the lower circumference being described by a greater radius than the radius of the upper circumference, a cabin floor at the intersection of these circumferences, the nose portion at its front end including such end being inclined downwardly for thereby decreasing the height of the aircraft and increasing the number of seats in a row, and engines under the middle portion of the wing.

REFERENCES:
patent: 2623720 (1952-12-01), Fortunato
Jame's All the World's Aircraft, 1968-1969, pp. 433-434, "Tupolev Tu-144."
Jame's All the World's Aircraft, 1969-1970, pp. 498-499, "Tupolev tu-144."
Jame's All the World's Aircraft, 1969-1970, pp. 403-404, "Northrup F-5A."
Jame's All the World's Aircraft, 1964-1965 p. 267, "North American RA-5C."

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