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- [31] INVESTIGATION OF COMBUSTOR-TURBINE-INTERACTION IN A ROTATING COOLED TRANSONIC HIGH-PRESSURE TURBINE TEST RIG: PART 1-EXPERIMENTAL RESULTS PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 2B, 2019,
- [32] EXPERIMENTAL INVESTIGATION OF SYNCHRONOUS FLOW INDUCED BLADE VIBRATIONS ON A RADIAL TURBINE - PART 1: NOMINAL INLET GUIDE VANE PROCEEDINGS OF ASME TURBO EXPO 2023: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2023, VOL 11A, 2023,
- [34] PHYSICS GUIDED GRAPH NEURAL NETWORKS (PG-GNNS): NUMERICAL INVESTIGATION OF HIGH-PRESSURE TURBINE FLOW PROCEEDINGS OF ASME TURBO EXPO 2024: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2024, VOL 12D, 2024,
- [35] HEAT TRANSFER FOR THE FILM-COOLED VANE OF A 1-1/2 STAGE HIGH-PRESSURE TRANSONIC TURBINE - PART II: EFFECT OF COOLING VARIATION ON THE VANE AIRFOIL AND INNER ENDWALL PROCEEDINGS OF THE ASME TURBO EXPO 2011, VOL 5, PTS A AND B, 2012, : 1735 - 1744
- [37] Secondary flow visualization on stagnation row of a combined impingement and film cooled high-pressure gas turbine nozzle guide vane using PIV technique Journal of Visualization, 2017, 20 : 817 - 832
- [38] EFFECTS OF TIP ENDWALL CONTOURING ON THE 3-DIMENSIONAL FLOW FIELD IN AN ANNULAR TURBINE NOZZLE GUIDE VANE .2. NUMERICAL INVESTIGATION JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1986, 108 (02): : 426 - 428
- [40] Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine-Part II: Effect of Cooling Variation on the Vane Airfoil and Inner End Wall JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2013, 135 (02):