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.
Month in the Patent Office
Aircraft Engineering and Aerospace Technology ; 32 , 12 ; 377
01.12.1960
1 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Emerald Group Publishing | 1958
Emerald Group Publishing | 1957
Emerald Group Publishing | 1957
Emerald Group Publishing | 1957
Emerald Group Publishing | 1956