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  • ProJet 2500
  • 공학설계D/B

    공학설계D/B 게시판 내용
    Volume Title Aerodynamics
    Volume No AEROFOILS AND WINGS - General. Aerofoils at subcritical speeds - lift, pitching moment.
    DATA Title Aerodynamic characteristics of aerofoils in compressible inviscid airflow at subcritical Mach numbers.
    DATA Item 72024
    KEYWORD aerodynamic, aerofoil, airfoil, angle, attack, center, centre, curve, incidence, lift, moment, pitching, slope, zero
    ISBN 0 85679 023 0
    ABSTRACT ESDU 72024 provides a means of estimating the lift-curve slope at zero lift, zero-lift incidence, zero-lift pitching moment coefficient and chordwise location of the aerodynamic centre for any aerofoil in compressible inviscid airflow from a knowledge of a number of parameters characterising the thickness distribution and camber line shape. The data, which are presented in graphical form, were derived by correlatng the results of a large number of calculations obtained from exact theory. - - - - - - - - - - - - - - -

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