In a high-pressure turbine that is used in combination with a contrarotating low-pressure
turbine, the geometry of the low-pressure turbine guide vane gives rise to a shock reflection …

摘要为降低以气流加速为主要做功手段的零预旋涡轮动叶激波损失, 提出了以折转角为控制变量
的吸力面无遮盖段内凹型线量化设计方法. 根据激波等强度时波系总损失最小的原理 …

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Periodic unsteadiness is inherent to flows in gas turbine engines, and in consequence very
many studies have been devoted to the understanding of unsteady flows in turbomachines …

This thesis presents a computational fluid dynamic (CFD) study of high pressure gas turbine
blade design with different realistic inlet temperature and velocity boundary conditions. The …

跨声速涡轮叶栅激波损失控制方法 主办:中国航空学会 北京航空航天大学 微信公众号 网站二维码
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