Reduction of end wall loss in axial compressor by using non-axisymmetric profiled end wall: A new design approach based on end wall velocity modification

Three-Dimensional Separations in Axial Compressors

Semiu A. Gbadebo, N. A. Cumpsty, Tom Hynes · Journal of Turbomachinery · 2005 · 274 citations

Engineering, Aerospace Engineering, Aerodynamics +14

A Criterion for Axial Compressor Hub-Corner Stall

Vai-Man Lei, Z. S. Spakovszky, E. M. Greitzer · Journal of Turbomachinery · 2008 · 207 citations

Engineering, Aerospace Engineering, Computational Engineering +13

Control of Three-Dimensional Separations in Axial Compressors by Tailored Boundary Layer Suction

Semiu A. Gbadebo, N. A. Cumpsty, Tom Hynes · Journal of Turbomachinery · 2007 · 143 citations

Engineering, Aerospace Engineering, Aerodynamics +15

Nonaxisymmetric Turbine End Wall Design: Part II—Experimental Validation

Jonathan Hartland, D. G. Gregory-Smith, N. W. Harvey et al. · Journal of Turbomachinery · 1999 · 134 citations · Full text

Engineering, Aerospace Engineering, Aerodynamics +13

Effects of Vortex Generator Application on the Performance of a Compressor Cascade

Alexander Hergt, Robert K. Meyer, Karl Engel · Journal of Turbomachinery · 2012 · 119 citations

Engineering, Aerospace Engineering, Mechanical Engineering +15