Method for analyzing flow losses in turobmachinery by using the measured results of stereoscopic particle image velocimetry
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Method for analyzing flow losses in turobmachinery by using the measured results of stereoscopic particle image velocimetry
Vol. 24, Issue 11, (2009)
作者机构:
北京航空航天大学能源与动力工程学院航空发动机气动热力科技重点实验室,北京,100191
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Published:2009
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LIU Bao-jie, YU Xian-jun, JIANG Hao-kang. Method for analyzing flow losses in turobmachinery by using the measured results of stereoscopic particle image velocimetry[J]. 2009, 24(11).
DOI:
LIU Bao-jie, YU Xian-jun, JIANG Hao-kang. Method for analyzing flow losses in turobmachinery by using the measured results of stereoscopic particle image velocimetry[J]. 2009, 24(11).DOI:
Method for analyzing flow losses in turobmachinery by using the measured results of stereoscopic particle image velocimetry
A method to calculate the entropy production rate based on the measured velocity flow fields was established based on the similar processes between stereoscopic particle image velocimetry(SPIV)measurement and large eddy simulation(LES).Comparing the turbulence dissipation rate estimated by several typical subgrid-scale(SGS) stress models
it can be found that the result calculated by the mixing model is most reasonable;however
the coefficients CSm and CAm should be well determined.Using the mixing model the entropy production rate of the complex flow fields near the rotor tip region measured by SPIV were analyzed.The results show that at the design condition the losses are mainly caused by the tip leakage vortex
while at the near-stall condition both the tip leakage vortex and the corner vortex can bring large flow losses.