타이틀 |
An Experimental Study of High-speed Counter-rotation Propeller on Low Speed Wind Range |
저자 |
UDF 공동연구팀 |
Keyword |
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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 |