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기술보고서

기술보고서 게시판 내용
타이틀	Separated Core Turbofan Engine
저자	Yoshio SAITO, Masanori ENDO, Yukio MATSUDA, Nanahisa SUGIYAMA, Noboru SUGAWARA, Kazuomi YAMAMOTO
Keyword	Ultrahigh bypass; Tubofan engine; Separated core
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr01289.pdf?id=NALTR0001289
보고서번호	NAL TR-1289
발행년도	1996.4
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	A new concept for a turbofan engine called the”Separated Core Turbofan Engine”is proposed and studied under the research program of the ultrahigh bypass turbofan engine for the next generation high-subsonic transport aircraft.The concept engine consists of two subunits,a core engine and a fan engine which are separate from each other.The results of the conceptual study show that this engine has many potential advantages over the corrent turbofan engines in many respects,inc