An airplane having a fuselage (11), opposed main wings (12), and blunt- leading-edge raked wingtips (8) is provided. Each main wing includes an outboard end (9) and a leading edge (14) having an outboard end leading-edge nose and nose radius. One blunt raked wingtip (8) is located at each main wing outboard en d (9) and includes a leading edge (20) swept back from the main wing leading edge (14). Each blunt raked wingtip (8) further includes a plurality of local airfoils each having a leading-edge nose radius and a chord. The nose radius is greater than abou t 2% of the local chord for the majority of the airfoils. The relative bluntness of the raked wingtips minimizes boundary-layer separation, drag associated with boundary- layer separation, and premature buffeting of the aircraft during low speed flight.
申请公布号
CA2291275(C)
申请公布日期
2007.11.06
申请号
CA19982291275
申请日期
1998.06.12
申请人
THE BOEING COMPANY
发明人
HOFFMAN, MICHAEL S.;PAUL, BERNARD P., JR.;WELLS, STEPHEN L.;BAYS-MUCHMORE, C. BYRAM;HERRICK, LARRY L.;VISSER, KENNETH D.;OGG, STEVEN S.;LEGRAND, LOUIS L.