| Effect of cavity depth on thermal performance of a cooled blade tip under rotation S Sakaoglu, HS Kahveci International Journal of Heat and Mass Transfer 143, 118561, 2019 | 30 | 2019 |
| Effect of Turbine Blade Tip Cooling Configuration on Tip Leakage Flow and Heat Transfer S Sakaoglu, HS Kahveci Journal of Turbomachinery 142 (2), 2020 | 20 | 2020 |
| Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine—Part I: Experimental Configuration and Data Review With Inlet Temperature Profile Effects HS Kahveci, CW Haldeman, RM Mathison, MG Dunn Journal of turbomachinery 135 (2), 2013 | 18 | 2013 |
| An optimization study for rotorcraft avionics bay cooling A Akin, HS Kahveci Aerospace Science and Technology 90, 1-11, 2019 | 15 | 2019 |
| Effect of turbulence modeling for the prediction of flow and heat transfer in rotorcraft avionics bay A Akin, HS Kahveci Aerospace Science and Technology 95, 105453, 2019 | 9 | 2019 |
| 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 HS Kahveci, CW Haldeman, RM Mathison, MG Dunn Journal of turbomachinery 135 (2), 2013 | 9 | 2013 |
| Implementation of a Stereoscopic PIV in Rotating Machinery Including Helicopter Rotor Flows HS Kahveci Pennsylvania State University, 2004 | 7 | 2004 |
| Effect of Turbine Blade Tip Cooling Configuration on Tip Leakage Flow and Heat Transfer S Sakaoglu, HS Kahveci Turbo Expo: Power for Land, Sea, and Air 58646, V05AT12A001, 2019 | 6 | 2019 |
| Validation of MISES 2-D Boundary Layer Code for High Pressure Turbine Aerodynamic Design PL Andrew, HS Kahveci Turbo Expo: Power for Land, Sea, and Air 47950, 879-893, 2007 | 6 | 2007 |
| Investigation of a rotor blade with tip cooling subject to a nonuniform temperature profile HS Kahveci Journal of Turbomachinery 143 (7), 2021 | 5 | 2021 |
| Airfoil and method for manufacturing an airfoil MA Jones, AE Smith, HS Kahveci US Patent App. 13/600,717, 2014 | 5 | 2014 |
| Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine: Part I—Experimental Configuration and Data Review With Inlet Temperature Profile Effects HS Kahveci, CW Haldeman, RM Mathison, MG Dunn Turbo Expo: Power for Land, Sea, and Air 54655, 1719-1733, 2011 | 5 | 2011 |
| 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 HS Kahveci, CW Haldeman, RM Mathison, MG Dunn Turbo Expo: Power for Land, Sea, and Air 54655, 1735-1744, 2011 | 5 | 2011 |
| The Influence of Film Cooling and Inlet Temperature Profile on Heat Transfer for the Vane Row of a 1-1/2 Stage Transonic High-Pressure Turbine HS Kahveci The Ohio State University, 2010 | 4 | 2010 |
| Flow around helicopter blade tip sections using 2D particle image velocimeter-part I HS Kahveci, C Camci 11th International Symposium on Transport Phenomena and Dynamics of Rotating …, 2006 | 4 | 2006 |
| Uncertainty Analysis of Heat Transfer Predictions Using Statistically Modeled Data From a Cooled 1-1/2 Stage High-Pressure Transonic Turbine HS Kahveci, KR Kirtley Journal of Turbomachinery 136 (6), 2014 | 3 | 2014 |
| Validation of MISES Two-Dimensional Boundary Layer Code for High-Pressure Turbine Aerodynamic Design PL Andrew, HS Kahveci Journal of turbomachinery 131 (3), 2009 | 3 | 2009 |
| Flow Around Helicopter Blade Tip Sections Using a (3D) Stereoscopic Particle Image Velocimeter—Part II HS Kahveci, C Camci 11th International Symposium on Transport Phenomena and Dynamics of Rotating …, 2006 | 3 | 2006 |
| Use of Artificial Neural Network in Rotorcraft Cooling System. A AKIN, HS Kahveci Journal of Aeronautics & Space Technologies/Havacilik ve Uzay Teknolojileri …, 2019 | 1 | 2019 |
| Comparison of Temperature Profile and Heat Transfer Predictions With Statistically-Modeled Data From a Cooled 1-1/2 Stage High-Pressure Transonic Turbine HS Kahveci, KR Kirtley Turbo Expo: Power for Land, Sea, and Air 55164, V03CT14A001, 2013 | 1 | 2013 |
