涵道比 / Bypass ratio – 中英文维基百科词条融合

By cathayvista航空

中文词条原文链接（无法从中国内地访问）：请点击这里访问
英文词条原文链接（无法从中国内地访问）：请点击这里访问
本文基于英文词条的线索，并补充部分来自中文词条的内容（在二者冲突时，以更晚更新者为准）。辽观搬运时进行了必要的合规化处理，以使其能够在中国内地上传。

维基百科（Wikipedia）是美国维基媒体基金会的互联网百科项目，其内容可能受到立场、信息来源等因素影响，请客观看待。正文内容不代表译者观点。 辽观提供的翻译仅供参考。文中可能包含无法从中国内地访问的链接。

辽观所搬运的词条文本与维基百科一道同样遵循CC BY-SA 4.0协议（辽观搬运的中英文对照版本），在符合协议要求的情况下您可以免费使用其内容（包括商用）。图片和视频可能遵循不同的共享协议。请点击这里访问

封面图片：涡轮发动机原理图。高涵道比(顶图)有一个大风叶，它绕着涡轮机输送大量空气；低涵道比(中图)有一个较小的风叶将更多的空气输送到涡轮机；涡轮喷气机(底图)无旁通道，所有的空气都通过涡轮机。
图片作者：Emoscopes 此图片遵循CC BY 2.5协议

1. 正文（发布于知乎专栏）

点击这里访问原文链接

2. 参考文献（仅英文词条，中文词条未列出参考文献）

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