국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Wind tunnel Investigation of an STOL Aircraft Model (An effefct of engine nacelle shape)
저자	wind Tunnel Investigation of an STOL Aircraft Model (An effefct of engine nacelle shape
Keyword	Engine nacelle; STOL aircraft model; Wind tunnel test
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltm00653.pdf?id=NALTM0000653
보고서번호	NAL TM-653
발행년도	1993.1
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	In initial wind tunnel tests on STOL experimental aircraft developed and researched by the National Aerospace Laboratory, a simulator engine nacelle which is longer and larger than that of 8％ scales of FJR engines used in actual aircraft, was installed and tested on a model. To estimate ASKA′s aerodynamics force data from wind tunnel data, the data