It is envisaged to arrange curved guide blades resembling Grothues spoilers in front of the ring nozzle on the ship's outer skin. Consequently, the guide blade has an entry tangent corresponding to the entry of a local boundary layer flow as downdraft, and has an exit tangent which is directed essentially orthogonally with respect to the entry plane of the ring nozzle. <IMAGE>
申请公布号
DE4025339(A1)
申请公布日期
1992.02.13
申请号
DE19904025339
申请日期
1990.08.10
申请人
SCHNEEKLUTH, HERBERT, PROF. DR.-ING., 5100 AACHEN, DE
发明人
SCHNEEKLUTH, HERBERT, PROF. DR.-ING., 5100 AACHEN, DE