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  • 기술보고서

    기술보고서 게시판 내용
    타이틀 An Experimental Study of High-speed Counter-rotation Propeller on Low Speed Wind Range
    저자 UDF 공동연구팀
    Keyword
    URL http://send.nal.go.jp/send/jpn/dlfile.php3/naltr0001326.pdf?doctype=7&filetype=20&path0=naltr0001326.pdf&path1=&path2=
    보고서번호 NAL TR-1326
    발행년도 1997.3
    출처 NAL (National Aerospace Laboratory of Japan)
    ABSTRACT A collaborative research project between the National Aerospace Laboratory and Japan Aircraft Development Company entitled “Wind tunnel testing of aircraft with advanced propeller in low-speed wind tunnel” was conducted from 1988 to 1992.This paper summarizes a series of experiments conducted on the counter-rotation type advanced turboprop propeller(CRP)under this project.The contents of the project were the development of a propeller test rig driven by an airturbine,measurement of the thrust characteristics of the 8blades CR

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