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轴流压缩系统失速可恢复性的预测
引用本文:吴艳辉,刘志伟,朱俊强,楚武利.轴流压缩系统失速可恢复性的预测[J].航空动力学报,2002,17(3):323-326.
作者姓名:吴艳辉  刘志伟  朱俊强  楚武利
作者单位:西北工业大学,航空动力与热力工程系,陕西,西安,710072
基金项目:国家自然科学基金资助项目 (5 98760 3 3 ),航空科学基金资助项目 (0 0 C5 3 0 2 7)
摘    要:基于描述轴流压气机及其系统的动态气动响应的一维非定常单元容积模型 ,通过数值求解并利用可视化的编程方法 ,模拟了单级、三级和九级压缩系统的失速可恢复性。单级压缩系统的数值模拟结果取得了实验结果的验证 ,九级压缩系统的数值模拟结果与该压缩系统在台架上的实际工作情况符合得很好 ,数值模拟结果揭示出了影响压缩系统失速恢复性的一些因素

关 键 词:轴流压缩系统  失速恢复性  数值模拟
文章编号:1000-8055(2002)03-0323-04
收稿时间:2001/5/14 0:00:00
修稿时间:2001年5月14日

The Predication of Stalling Recoverability of the Compression Systems
WU Yan hui,LU Zhi wei,ZHU Jun qiang and CHU Wu li.The Predication of Stalling Recoverability of the Compression Systems[J].Journal of Aerospace Power,2002,17(3):323-326.
Authors:WU Yan hui  LU Zhi wei  ZHU Jun qiang and CHU Wu li
Institution:Northwestern Polytechnical University,Xi'an710072,China;Northwestern Polytechnical University,Xi'an710072,China;Northwestern Polytechnical University,Xi'an710072,China;Northwestern Polytechnical University,Xi'an710072,China
Abstract:The stalling recoverability of one stage,three stage and nine stage axial flow compression systems is simulated based on a one dimensional unsteady stage by stage model for the dynamic response of a compression system.The validation of the model is verified by good agreement between the simulation results and experimental results in the single stage and nine stage compression systems.The simulation results also point out that some factors (such as in stall stage characteristic,the volume of plenum and compressor shaft speed) affect the stalling recoverability of axial flow compression systems to some extent.Stage matching can have a significant effect on stalling recoverability in high speed multistage compressors.
Keywords:axial  flow compression system  stalling recoverability  numerical simulation
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