본문 바로 가기

로고

국내 최대 기계 및 로봇 연구정보
통합검색 화살표
  • ProX 300  메탈3D 프린터
  • 공학설계D/B

    공학설계D/B 게시판 내용
    Volume Title Aerodynamics
    Volume No WING-BODY COMBINATIONS - Lift, normal force, pitching moment, aerodynamic centre, upwash
    DATA Title Aerodynamic centre of wing-fuselage-nacelle combinations: effect of wing-pylon mounted nacelles.
    DATA Item 77012
    KEYWORD aerodynamic, body, centre, combination, fuselage, nacelle, pylon, wing, center
    ISBN 0 85679 183 0
    ABSTRACT ESDU 77012 gives a method for estimating the forward shift of aerodynamic centre by treating the nacelle as an annular wing of diameter equal to the nacelle spanwise width. A graph gives the lift-curve slope for an annular wing as a function of its width to length ratio, the lift is assumed to act at the nacelle lip, and a correction term for the effect of the wing upwash field is added. The method is validated by comparing predictions with wind-tunnel data taken from the literature for both free-flow nacelles and nacelles with variable mass flow and is found to predict the shift to within 0.02 of mean aerodynamic chord. The wing lift-curve slope, also required in the method, is obtained from ESDU 70011 and the aerodynamic centre of the wing-fuselage combination, to which the forward shift is applied, is obtained from ESDU 76015.

    서브 사이드

    서브 우측상단1