국내 최대 기계 및 로봇 연구정보

공학설계D/B

공학설계D/B 게시판 내용
Volume Title	Aerodynamics
Volume No	CONTROLS AND FLAPS - Flaps - lift curve, pitching moment. Flaps - drag.
DATA Title	Conversion factor for profile drag increment for part-span flaps.
DATA Item	Aero F.02.01.07
KEYWORD	aileron, device, drag, elevator, flap, high, lift, plain, profile, rudder, slotted, split
ISBN
ABSTRACT	ESDU Aero F.02.01.07 gives curves that provide factors to correct the profile drag increment due to deflection of a full-span flap to give the increment for a part-span flap with arbitrary spanwise position. The curves are a function of taper ratio and apply to straight-tapered wings. They may be used with the full-span increments from ESDU 74010 for split flaps, from ESDU 87024 for plane flaps, and from ESDU 87005 for single-slotted flaps.