국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	The First Estimations of Wind tunnel Uncertainties for HOPE
저자	Takeo AOKI, Koichi SUZUKI, Nobuyuki HOSOE, Seigo NAKAMURA, Masami MATSUDA, Jun TAKANO
Keyword	spacecraft; wind tunnel uncertainty; tolerance
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltm00704.pdf?id=NALTM0000704
보고서번호	NAL TM-704
발행년도	1996.11
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	The H-2 Orbiting Plane (HOPE) launched by an H-2 rocket or its derivative, is being studied by the National Aerospace Laboratory (NAL) and the National Space Development Agency of Japan (NASDA). Wind tunnel tests were performed using the same HOPE 2.5％ scale model using the same balance and sting as the first step in developing wind tunnel uncertainities for HOPE. NAL 2m×2m Transonic Wind Tunnel and KHI 1m×1m Transonic Wind Tunnel which belongs to Kawasaki Heavy Industrie similar to HOPE, can be available in developing tolerances for HOPE, from comparison of tolerances between present wind tunnel test data and the past HOPE series wind tunnel test data.