Investigation on the Forced Response of a Radial Turbine under Aerodynamic Excitations
文献类型:期刊论文
作者 | Ma, C. C., Huang, Z. and Qi, M. X.1 |
出版日期 | 2016 |
关键词 | radial turbine forced response aerodynamic excitation FSI SAFE diagram Thermodynamics Engineering |
中文摘要 | In order to investigate the effects of probe support on the stall characteristics of micro compressors, an experiment was carried out on a large-scale low-speed research compressor according to the principle of geometric similarity. A cylindrical probe support intruding to 50% blade span was mounted at 50% chord upstream from the rotor blade leading edge. The static pressure rise characteristic of the compressor is measured, with and without the probe support respectively. The dynamic compressor behavior from pre-stall to full stall was also measured. The results indicate that the stability margin of the compressor is lowered after installing the probe support. The stall inception is aroused by modal wave disturbances. The disturbances developed into two stall cells smoothly before installing the probe support, while the disturbances first developed into a single stall cell then splitting into two stall cells after installing the probe support. The presence of probe support lowers the initial intensity of the rotating stall of the compressor, while it doesn't alter the intensity of the rotation stall after the compressor enters into full stall. |
源URL | [http://ir.etp.ac.cn/handle/311046/113087] ![]() |
专题 | 工程热物理研究所_Journal of Thermal Science_期刊论文 |
作者单位 | 1.[Ma Chaochen 2.Huang Zhi 3.Qi Mingxu] Beijing Inst Technol, Sch Mech Engn, Beijing 100081, Peoples R China. |
推荐引用方式 GB/T 7714 | Ma, C. C., Huang, Z. and Qi, M. X.. Investigation on the Forced Response of a Radial Turbine under Aerodynamic Excitations[J],2016. |
APA | Ma, C. C., Huang, Z. and Qi, M. X..(2016).Investigation on the Forced Response of a Radial Turbine under Aerodynamic Excitations.. |
MLA | Ma, C. C., Huang, Z. and Qi, M. X.."Investigation on the Forced Response of a Radial Turbine under Aerodynamic Excitations".(2016). |
入库方式: OAI收割
来源:工程热物理研究所
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