Investigation on centrifugal impeller in an axial-radial combined compressor with inlet distortion
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-011-0500-7.pdf
Reference20 articles.
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3. Halstead, D. E., Wisler, D. C., Okiishi, T. H., et al. Boundary Layer Development in Axial Compressors and Turbines: part 1 of 4-Composite Picture. ASME, Journal of Turbomachinery, 1997, 119(1), 114–127.
4. Ernst, M., Michel, A. and Jeschke, P. Analysis of Rotor-Stator-Interaction and Blade-to-Blade Measurements in a Two Stage Axial Flow Compressor. ASME, Journal of Turbomachinery, 2011, 133(1), 011–027.
5. Sanders, A. J., Fleeter, S. Rotor Blade-to-blade Wake Variability and Effect on Downstream Vane Response. AIAA, Journal of Propulsion and Power. 2002, 18(2), 456–464.
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