An aerofoil wing comprising upper and lower surfaces meeting at the leading and trailing edges and a camber line representing the curvature of the aerofoil comprising at least two regions of substantially linear increases in curvature and wherein the increases in curvature are of monotonically increasing magnitude. Preferably there are three regions of substantially linear increases in curvature.
申请公布号
WO0038984(A1)
申请公布日期
2000.07.06
申请号
WO1999GB03434
申请日期
1999.10.15
申请人
THE SECRETARY OF STATE FOR DEFENCE;HACKETT, KEVIN, CHRISTOPHER;ASHILL, PATRICK, RALPH;GREEN, JOHN, EDWARD
发明人
HACKETT, KEVIN, CHRISTOPHER;ASHILL, PATRICK, RALPH;GREEN, JOHN, EDWARD