Month in the Patent Office

Abstract

The fore‐body of the aircraft described in the parent Specification is, in plan form, a finely pointed triangle A B B in which the leading edges D, D lie within the straight lines D1, D1 joining the bow to the ends of the base, thereby obtaining a low thickness/chord ratio without increase in drag.

Citation

(1960), "Month in the Patent Office", Aircraft Engineering and Aerospace Technology, Vol. 32 No. 12, pp. 377-377. https://doi.org/10.1108/eb033349