| 摘要 |
The present invention relates to a noise supressor assembly for a jet engine comprised of a plurality of conduit assemblies proximate the trailing edges of the wall members which capture a portion of an ambient gaseous stream flowing in an ambient flow for introduction into the hot core gaseous flow to thereby deform the interface between the hot core flow and the fan flow or ambient flow when there is no fan between the fan flow and the ambient flow or between fully or partially mixed core and fan flows and the ambient flow thereby mixing such gaseous streams to thereby reduce velocity of the hot core and fan flows and thus jet noise level.
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