본문 바로 가기

로고

국내 최대 기계 및 로봇 연구정보
통합검색 화살표
  • 시편절단기 EVO 500
  • 기술보고서

    기술보고서 게시판 내용
    타이틀 Estimation of Cable-Mounted Model Inertia Characteristics for Dynamic Wind-Tunnel Test
    저자 Masaaki YANAGIHARA, Masahiko NAGAYASU, Shuichi SASA, Takashi Shimomura
    Keyword moment of inertia; cable-mounted model; bifilar pendulum
    URL http://send.nal.go.jp/send/jpn/dlpdf.php3/naltm00641.pdf?id=NALTM0000641
    보고서번호 NAL TM-641
    발행년도 1991.10
    출처 NAL (National Aerospace Laboratory of Japan)
    ABSTRACT The inertia characteristics of a National Aerospace Laboratory (NAL) Spaceplane cable-mounted model (1:20) used for dynamic wind tunnel tests were experimentally estimated. The estimated parameters consisted of the vertical position of the model′s center of gravity, the inertia moments Ix, Iy and Iz, and the product of inertia Ixz. The method was based on a bifilar pendulun system and estimation errors were evaluated. As a result, the moment of inertia Iy and Iz were estimated within an about ±1% error, although Ix and t

    서브 사이드

    서브 우측상단1