Effects of labyrinth cavity angles and non-axisymmetric end wall on the performance of the shrouded stator at different inlet boundary layer thicknesses
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DOI: 10.1063/5.0286356
Abstract: The interplay between leakage flow and secondary flow markedly impairs the aerodynamic efficacy of shrouded stators within axial compressors. However, the synergistic influence of inlet boundary layer thickness, cavity angles, and non-axisymmetric end wall contouring… read more here.
Keywords: cavity; non axisymmetric; end wall; axisymmetric end ... See more keywords