Influence of Cavity Leakage flow on Corner Separation in a Shrouded Stator Cascade

The Influence of Shrouded Stator Cavity Flows on Multistage Compressor Performance

Steven R. Wellborn, T. H. Okiishi · Journal of Turbomachinery · 1999 · 79 citations

Engineering, Aerospace Engineering, Aerodynamics +12

Control of corner separation via dimpled surface for a highly loaded compressor cascade under different inlet Mach number

Huawei Lu, Yi Yang, Shuang Guo et al. · Aerospace Science and Technology · 2018 · 51 citations

Engineering, Aerospace Engineering, Aerodynamics +13

The Aerodynamic Interaction of Stator Shroud Leakage and Mainstream Flows in Compressors

A. A. J. Demargne, John P. Longley · Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery · 2000 · 50 citations

Engineering, Aerospace Engineering, Mechanical Engineering +15

Effect of the Stator Hub Configuration and Stage Design Parameters on Aerodynamic Loss in Axial Compressors

Sungho Yoon, Rudolf Selmeier, Patricia Cargill et al. · Journal of Turbomachinery · 2015 · 45 citations

Engineering, Aerospace Engineering, Aerodynamics +12

Three-dimensional unsteady simulation of a multistage axial compressor with labyrinth seals and its effects on overall performance and flow characteristics

Sangjo Kim, Kuisoon Kim, Changmin Son · Aerospace Science and Technology · 2019 · 39 citations

Engineering, Physics, Aerodynamics +16