Volume 32 Issue 5
May  2017
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Performance prediction model of partial casing treatment[J]. Journal of Aerospace Power, 2017, 32(5): 1207-1215. doi: 10.13224/j.cnki.jasp.2017.05.022
Citation: Performance prediction model of partial casing treatment[J]. Journal of Aerospace Power, 2017, 32(5): 1207-1215. doi: 10.13224/j.cnki.jasp.2017.05.022

Performance prediction model of partial casing treatment

doi: 10.13224/j.cnki.jasp.2017.05.022
  • Received Date: 2015-09-23
  • Publish Date: 2017-05-28
  • Using the idea of inlet distortion parallel compressor theory dividing the compressor into some sub compressors, the partial casing treatment compressor was divided into casing treatment sub compressor and solid wall sub compressor. Then the outlet parameter of the partial casing treatment compressor was got according to the laws of momentum conservation and energy conservation, and the assumption of partial casing treatment performance prediction model was acquired based on the experimental conclusions of linear relationship between the mass flow of stall margin point and the casing treatment circumferential angle. Comparisons of the prediction results and the experimental results reveal that the curves of prediction characteristics and experimental characteristics are consistent in overall trend. Under supersonic condition at 98% design rotating speed, the peak efficiency prediction error is smaller than 0.5%, and the comprehensive margin prediction error is under 0.6%.

     

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