| 摘要 |
<p>The invention relates to a turbojet engine with reduced noise emission. Said turbojet engine (1) is configured in the form of double-tube engine comprising an inner flow channel (14) and an outer flow channel (12), the inner flow channel (14) being covered by said outer flow channel (12). A main flow (11) is guided in the outer flow channel (12), while an auxiliary flow (13) is guided in the inner flow channel (14).</p> |
