국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Identifying the NAL Spaceplane Aerodynamic Model using Dynamic Wind Tunnel Tests
저자	Dynamic Wind Tunnel Test Group
Keyword	cable mount; dynamic wind tunnel test; parameter identification
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr01171.pdf?id=NALTR0001171
보고서번호	NAL TR-1171
발행년도	1992.7
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	An aerodynamic model identification technique utilized by the National Aerospace Laboratory(NAL)was applied to dynamic wind tunnel tests using a cable mounted model to extract aerodynamic parameters of the NAL Spaceplane.The estimated static parameters were evaluated by comparisons with static wind tunnel test results,whereas those for the dynamic parameters with theoretically estimated values.In addition,mathematical flight simulations using both static and dynamic parameters w