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喷气推进/热力循环/涡扇循环
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来自维基教科书,面向开放世界的开放教材
<
喷气推进
|
热力循环
风扇通过较大的质量流来抵消平均排气速度,藉此可降低给定推力。
现代军用飞机会采用加力燃烧,同时汇合旁路和核心流量以实现高增比。
此页面或章节是一个未完成的草稿或大纲。
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书籍:喷气推进
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华夏公益教科书