국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Model with Turbine Powered Simulators at NAL's Low Speed Wind Tunnel Facility
저자	Teruomi Nakatani, Osamu Nonaka, Katsuichi Murota, Hiroshi Kondou, Yoshio Hayashi
Keyword	Wind Tunnel Test System; Turbine Powered Simulator; Piping Interference System; Air Bearing
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr0001421.pdf?id=NALTR0001421
보고서번호	NAL TR-1421
발행년도	2000.12
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	This paper describes a test system of an 8% scale model of STOL aircaft ?SKA?with turbine powered simulators tested at the Low Speed Wind Tunnel (6.5m x 5.5m) of National Aerospace Laboratory (NAL). The purpose of the system is to achieve high accurate measurements of aerodynamic forces by eliminating piping interferences. The paper also descibes performance of the piping interference elimination function and overall system test results.