국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Suspending Wind-Tunnel Test for the ALFLEX Vehicle
저자	Dynamic Wind Tunnel Test Group, NAL/NASDA HOPE Joint Team, ALFLEX Sub Group
Keyword	ALFLEX; HOPE; dynamic wind-tunnel test; Identification
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr01306.pdf?id=NALTR0001306
보고서번호	NAL TR-1306
발행년도	1996.9
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	A suspending wind-tunnel test for the Automatic Landing Flight Experiment (ALFLEX) was conducted as a part of the research on an unmanned winged re-entry vehicle (HOPE).The suspending flight was simulated in the wind-tunnel using a 40％ scaled model of the ALFLEX vehicle to validate the design of the suspending system and to identify the aerodynamic characteristics of the vehicle for designing a control system.As a result,problems of some eleme.The flight test plan of ALFLEX is then fixed on these results.