Articles | Volume 8, issue 1
https://doi.org/10.5194/ms-8-127-2017
© Author(s) 2017. This work is distributed under the Creative Commons Attribution 3.0 License.
Research article
| 
31 May 2017
Research article |
| 31 May 2017
Performance of a Low Speed Axial Compressor Rotor Blade Row under Different Inlet Distortions
Related subject area
Subject: Fluid Mechanics | Techniques and Approaches: Numerical Modeling and Analysis
Axial transonic compressor performance enhancement with circumferential grooves
Mech. Sci., 11, 153–161, 2020
Cited articles
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Charalambous, N., Ghisu, T., Iurisci, G., Pachidis, V., and Pilidis, P.: Axial compressor response to inlet flow distortions by a CFD analysis, ASME Turbo Expo, Power for Land, Sea, and Air, 5, 1637–1649, 2004.
Dong, X., Sun, D., Li, F., Jin, D., Gui, X., and Sun, X.: Effects of Rotating Inlet Distortion on Compressor Stability With Stall Precursor-Suppressed Casing Treatment, J. Fluid. Eng., 137, 111101, https://doi.org/10.1115/1.4030492, 2015.
Furukawa, M., Inoue, M., Saiki, K., and Yamada, K.: The role of tip leakage vortex breakdown in compressor rotor aerodynamics, ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition, 1998.
Hah, C., Rabe, D. C., Sullivan, T. J., and Wadia, A. R.: Effects of inlet distortion on the flow field in a transonic compressor rotor, J. Turbomach., 120, 233–246, https://doi.org/10.1115/1.2841398, 1998.
