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- [31] A Combined Numerical and Experimental Study of the Effect of Non-Axisymmetric Contouring on Performance and Film Cooling Behavior of a Rotating Turbine Endwall PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 5B, 2014,
- [32] Effects of inlet distortion and non-axisymmetric endwall modeling on performance of compact compressor intermediate duct Hangkong Dongli Xuebao/Journal of Aerospace Power, 2024, 39 (01):
- [34] MEASUREMENTS OF SECONDARY LOSSES IN A TURBINE CASCADE WITH THE IMPLEMENTATION OF NON-AXISYMMETRIC ENDWALL CONTOURING PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 6, PT A, 2008, : 1405 - 1417
- [35] Application of 3D blading and non-axisymmetric endwall in a transonic compressor Tuijin Jishu/Journal of Propulsion Technology, 2016, 37 (02): : 250 - 257
- [37] 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
- [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] Experimental Investigation of the Effect of Purge Flow on Film Cooling Effectiveness on a Rotating Turbine with Non-Axisymmetric Endwall Contouring PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2013, VOL 3B, 2013,
- [40] ADVANCED NON-AXISYMMETRIC ENDWALL CONTOURING FOR AXIAL COMPRESSORS BY GENERATING AN AERODYNAMIC SEPARATOR - PART I: PRINCIPAL CASCADE DESIGN AND COMPRESSOR APPLICATION PROCEEDINGS OF ASME TURBO EXPO 2009, VOL 7, PTS A AND B, 2009, : 113 - 120