국내 최대 기계 및 로봇 연구정보

공학설계D/B

공학설계D/B 게시판 내용
Volume Title	Aerodynamics
Volume No	AEROFOILS AND WINGS - Aerofoils at supersonic speeds. Critical Mach number and pressure coefficient. Flat plates.
DATA Title	Skin friction drag coefficients for a flat plate in two-dimensional flow with zero heat transfer.
DATA Item	Aero W.S.02.04.12
KEYWORD	aerofoil, drag, flow, profile, supersonic, airfoil
ISBN
ABSTRACT	ESDU Aero W.S.02.04.12 gives curves for the skin friction drag coefficient of a flat plate plotted against the fraction of the plate for which the boundary layer is laminar for values of freestream Mach number up to 5. Sets of curves are given for Reynolds numbers of one million, ten million and a hundred million. These curves should only be used in conjunction with ESDU Aero W.S.02.04.13, and, for more recent information concerning skin friction and other parameters for laminar and turbulent boundary layers on a smooth flat plate, ESDU 68019 and ESDU 68020 should be consulted.