The performance of the compression ramp are studied mostly at the design point and off-design point in the condition of uniform supersonic incoming flow, and slightly at the design point in the condition of non-uniform incoming flow.
文中主要研究了压缩面在均匀来流条件下设计点与非设计点的气动性能,也简略地分析了非均匀来流条件下设计点的气动性能。
参考来源 - 弯曲激波压缩面设计及试验研究·2,447,543篇论文数据，部分数据来源于NoteExpress
本文采用改进的流线曲率法对跨声速多级轴流压气机非设计点进行了性能模拟。
An improved streamline curvature numerical method is modified and applied to better approximate the flow fields of multi-stage transonic axial compressors.
本文采用改进的流线曲率法+对跨声速多级轴流压气机非设计点进行了性能模拟。
An improved streamline curvature numerical method is modified and applied to better approximate the flow fields of multi-stage transonic axial compressors.
对所设计的三种外形方案，计算了设计点和非设计点的气动性能，并对影响性能的因素进行了讨论。
The aerodynamic performances of on-design and off-design for the three conceptual configurations designed were computed, and the factors affected the performance were also discussed.
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