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국내 최대 기계 및 로봇 연구정보
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  • ProX 300  메탈3D 프린터
  • 공학설계D/B

    공학설계D/B 게시판 내용
    Volume Title Aerodynamics
    Volume No AEROFOILS AND WINGS - Wings - drag
    DATA Title Introductory sheet on subcritical lift-dependent drag of wings.
    DATA Item 66031
    KEYWORD camber, dependent, drag, induced, lift, profile, trailing, twist, vortex, wing
    ISBN
    ABSTRACT ESDU 66031 discusses the various contributions to the drag of a lifting wing of moderate to high aspect ratio in subcritical viscous flow, considering both a cambered and twisted wing and a plane symmetrical section wing. A method of analysis is discussed for the case of plane symmetrical section wings; it uses ESDU 74035 to determine the drag due to trailing vortices and applies a correction for lift dependent drag due to boundary layer developed in ESDU 66032.

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