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- [34] ADVANCED NON-AXISYMMETRIC ENDWALL CONTOURING FOR AXIAL COMPRESSORS BY GENERATING AN AERODYNAMIC SEPARATOR - PART II: EXPERIMENTAL AND NUMERICAL CASCADE INVESTIGATION PROCEEDINGS OF ASME TURBO EXPO 2009, VOL 7, PTS A AND B, 2009, : 121 - 131
- [35] THE AERODYNAMIC OPTIMIZATION DESIGN OF TURBINE CASCADE WITH NONAXISYMMETRIC ENDWALL AND EXPERIMENTAL VALIDATIONS PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2017, VOL 2A, 2017,
- [36] GENERATIVE MODEL BASED PARAMETERIZATION FOR MORE EFFICIENT AERODYNAMIC OPTIMIZATION OF NON-AXISYMMETRIC ENDWALL PROCEEDINGS OF ASME TURBO EXPO 2024: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2024, VOL 12D, 2024,
- [37] A NEW TEST FACILITY TO INVESTIGATE FILM COOLING ON A NON-AXISYMMETRIC CONTOURED TURBINE ENDWALL, PART I: INTRODUCTION AND AERODYNAMIC MEASUREMENTS ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2015, VOL 2A, 2015,
- [38] Numerical Investigation of the Effect of Purge Flow on Aerodynamic Performance and Film Cooling Effectiveness on a Rotating Turbine with Non-Axisymmetric Endwall Contouring PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 4, PTS A AND B, 2012, : 413 - 423
- [39] Application of non-axisymmetric endwall contouring to conventional and high-lift turbine airfoils Proceedings of the ASME Turbo Expo 2007, Vol 6, Pts A and B, 2007, : 653 - 661