본문 바로 가기

로고

국내 최대 기계 및 로봇 연구정보
통합검색 화살표
  • Virtuous6D
  • 기술보고서

    기술보고서 게시판 내용
    타이틀 Computations of FLow past Multi-Element Airfoils in Wind Tunnel
    저자 Masayoshi NAKAMURA, Koichi SUZUKI, Asao HANZAWA, Naoaki KUWANO
    Keyword Numerical flow analysis; Multi-element airfoil
    URL http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr01256.pdf?id=NALTR0001256
    보고서번호 NAL TR-1256
    발행년도 1995.1
    출처 NAL (National Aerospace Laboratory of Japan)
    ABSTRACT This paper presents an overview of numerical flow analyses past arbitrarily designed multi-element airfoils.Compressible unsteady inviscid flows aroung airfoils are analyzed by integrations of time-dependent Euler equations using finite difference tow around a symmetrical airfoil in a free-flight condition.Other calculations for a low-speed flow around a large thickness airfoil and variations with flap and spoiler were made in a wind tunnel boundary condition.Comparisons of pressure distributions and lift coefficients were also made with other calculated solutions and with experimental data.

    서브 사이드

    서브 우측상단1