국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Construction and Performance of a Tension Controlled Model Suspension System in the Low Speed wind Tunnel
저자	Masataka HASHIDATE, Hiroshi MATSUSHITA, Yasukatsu ANDO, Shigeo KAYABA, Kenji FUJII
Keyword	Wind tunnel test; Tension contrlled model suspension system; Tension control; Active control technology
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr01299.pdf?id=NALTR0001299
보고서번호	NAL TR-1299
발행년도	1996.7
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	A tension-controlled model suspension system was developed which is to be used in validation study of active control technology,giving a complete aircraft model a motion degree of freedom in the NAL Low-Speed Wind Tunnel.A torque motor on the tunnel celing suspends a model which moves along a rail vertically supported at the center enter position without going out of the test section.The system was successfully used in the wind tunnel tests for gust load alleviation of a complete aircraft aeroelastic model,and its effective functions were verified.This report described the structure,the performance,and applications of the system.