Engine so designed that all aircraft accessories are mounted on reduction gear rear case; arrangement favors frontal area at expense of oa length, and results in nacelle of good fineness ratio with extremely low drag; it weighs 1600 lb and delivers 3460 shp and 725 lb jet thrust at 13,800 rpm; test results.
Allison t56 turbo-prop aircraft engine
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1955 Turbine propeller
1955
14 pages
Aufsatz (Konferenz)
Englisch
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