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  • 진공함침기 Poly’vac
  • 공학설계D/B

    공학설계D/B 게시판 내용
    Volume Title Aerodynamics
    Volume No AEROFOILS AND WINGS - Wings - lift, pitching moment, aerodynamic centre, spanwise loading
    DATA Title Effect of cut-out on lift-curve slope.
    DATA Item Aero W.01.01.04
    KEYWORD curve, cut, lift, out, slope, wing
    ISBN
    ABSTRACT ESDU Aero W.01.01.04 presents curves of the ratio of the wing or tailplane lift-curve slope with cut-out to that without cut-out plotted against cut-out span as a fraction of wing or tailplane span for various values of cut-out chord as a fraction of wing or tailplane chord. A sketch indicates how the span and chord of the cut-out are defined. The curves are theoretically derived for a rectangular cut-out.

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