공학설계D/B

공학설계D/B 게시판 내용
Volume Title	Aerodynamics
Volume No	AEROFOILS AND WINGS - General. Aerofoils at subcritical speeds - lift, pitching moment.
DATA Title	Slope of lift curve for two-dimensional flow.
DATA Item	AERO W.01.01.05
KEYWORD	aerofoil, curve, lift, slope, airfoil
ISBN
ABSTRACT	ESDU AERO W.01.01.05 is retained in the Series because it is referred to and used in a number of ESDU documents in Aerodynamics. To obtain values of the slope of the lift coefficient curve with angle of attack on an aerofoil in incompressible (or compressible but subcritical) flow, ESDU 72024 and ESDU 97020 should be used.