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- [32] BLADE-ROW INTERACTION IN AN AXIAL-FLOW SUBSONIC COMPRESSOR STAGE JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1980, 102 (01): : 169 - 177
- [33] EFFECT OF HOT STREAK MIGRATION ON UNSTEADY BLADE ROW INTERACTION IN AN AXIAL TURBINE PROCEEDINGS OF THE ASME TURBO EXPO 2010: TURBOMACHINERY: AXIAL FLOW FAN AND COMPRESSOR AERODYNAMICS DESIGN METHODS, AND CFD MODELING FOR TURBOMACHINERY, VOL 7, PTS A-C, 2010, : 2573 - 2584
- [34] Effect of Hot Streak Migration on Unsteady Blade Row Interaction in an Axial Turbine JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2012, 134 (05):
- [36] NUMERICAL AND EXPERIMENTAL ANALYSIS OF THE EFFECTS OF NON-AXISYMMETRIC CONTOURED STATOR ENDWALLS IN AN AXIAL TURBINE PROCEEDINGS OF THE ASME TURBO EXPO 2010: TURBOMACHINERY: AXIAL FLOW FAN AND COMPRESSOR AERODYNAMICS DESIGN METHODS, AND CFD MODELING FOR TURBOMACHINERY, VOL 7, PTS A-C, 2010, : 1549 - 1559
- [38] Non-Axisymmetric stator Hub Endwall Contouring for Tandem Bladed Axial Compressor stage PROCEEDINGS OF ASME 2023 GAS TURBINE INDIA CONFERENCE, GTINDIA2023, 2023,
- [40] Aero-Thermal Coupled Design Optimization of the Non-Axisymmetric Endwall for a Gas Turbine Blade PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 2D, 2018,