An exit area control for a jet engine comprising a tubular member having an open end whose area is to be varied; a plurality of longitudinally extended louvres; means supported at each end of said tubular member to circumferentially dispose said louvres; means to rotatably support said louvres in said last-mentioned means; and means to rotatably adjust each louver on its longitudinal axis to thereby vary the effective area of said open end.
U.S. Patent Specifications
Aircraft Engineering and Aerospace Technology ; 24 , 9 ; 285-286
01.09.1952
2 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Emerald Group Publishing | 1960
Emerald Group Publishing | 1958
Emerald Group Publishing | 1958
Emerald Group Publishing | 1958
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