A research program of low bypass ratio small front fan engines has been in process at Third Research Center of Technical Research and Development Institure of Japan Defence Agency since 1975. The final target of this program is the development of the propulsion engine for the high subsonic small aircraft. As the first phase of this program, the bench test engine XF3-1 was manufactured and the basic studies of the overall engine matching performance and the effect of each component on the engine performance have been carried out. This paper describes the XF3-1 engine, reviews the status of the research and presents the major engineering progress attained through the research. (Kursetz)
Research of the XF3-1 turbofan engine
Forschungsarbeiten am Blaesertriebwerk XF3-1
ASME-Papers ; 1-7
1978
7 Seiten, 11 Bilder, 3 Tabellen
Conference paper
English
Springer Verlag | 2021
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