| Adiabatic and overall effectiveness for the showerhead film cooling of a turbine vane ML Nathan, TE Dyson, DG Bogard, SD Bradshaw Journal of Turbomachinery 136 (3), 031005, 2014 | 113 | 2014 |
| Effect of internal crossflow velocity on film cooling effectiveness—Part I: Axial shaped holes JW McClintic, JB Anderson, DG Bogard, TE Dyson, ZD Webster Journal of Turbomachinery 140 (1), 011003, 2018 | 103 | 2018 |
| Sensitivity of the overall effectiveness to film cooling and internal cooling on a turbine vane suction side RP Williams, TE Dyson, DG Bogard, SD Bradshaw Journal of Turbomachinery 136 (3), 031006, 2014 | 99 | 2014 |
| Adiabatic and Overall Effectiveness for a Fully Cooled Turbine Vane TE Dyson, JW McClintic, DG Bogard, SD Bradshaw Turbo Expo: Power for Land, Sea, and Air 55157, V03BT13A037, 2013 | 59 | 2013 |
| Overall effectiveness for a film cooled turbine blade leading edge with varying hole pitch TE Dyson, DG Bogard, JD Piggush, A Kohli Journal of turbomachinery 135 (3), 031011, 2013 | 58 | 2013 |
| Evaluation of CFD simulations of film cooling performance on a turbine vane including conjugate heat transfer effects TE Dyson, DG Bogard, SD Bradshaw International journal of heat and fluid flow 50, 279-286, 2014 | 37 | 2014 |
| Adiabatic and overall effectiveness for the showerhead film cooling of a turbine vane ML Nathan, TE Dyson, DG Bogard, SD Bradshaw Turbo Expo: Power for Land, Sea, and Air 44700, 1537-1547, 2012 | 33 | 2012 |
| Conjugate Heat Transfer Scaling for Inconel 718 WR Stewart, TE Dyson Turbo Expo: Power for Land, Sea, and Air 50879, V05AT10A007, 2017 | 26 | 2017 |
| Flow physics of diffused-exit film cooling holes fed by internal crossflow JW McClintic, DW Fox, FB Jones, DG Bogard, TE Dyson, ZD Webster Journal of Turbomachinery 141 (3), 031010, 2019 | 23 | 2019 |
| Freestream Flow Effects on Film Effectiveness and Heat Transfer Coefficient Augmentation for Compound Angle Shaped Holes JB Anderson, JW McClintic, DG Bogard, TE Dyson, Z Webster Turbo Expo: Power for Land, Sea, and Air 50893, V05CT19A027, 2017 | 23 | 2017 |
| Rib turbulator effects on crossflow-fed shaped film cooling holes DW Fox, FB Jones, JW McClintic, DG Bogard, TE Dyson, ZD Webster Journal of Turbomachinery 141 (3), 031013, 2019 | 20 | 2019 |
| Sensitivity of the overall effectiveness to film cooling and internal cooling on a turbine vane suction side RP Williams, TE Dyson, DG Bogard, SD Bradshaw Turbo Expo: Power for Land, Sea, and Air 44700, 1549-1557, 2012 | 19 | 2012 |
| Evaluation of CFD simulations of film cooling performance on a turbine vane including conjugate heat transfer effects TE Dyson, DG Bogard, SD Bradshaw Turbo Expo: Power for Land, Sea, and Air 44700, 1527-1535, 2012 | 18 | 2012 |
| Evaluation of CFD simulations of film cooling performance in the showerhead region of a turbine vane including conjugate effects TE Dyson, DG Bogard, SD Bradshaw ASME International Mechanical Engineering Congress and Exposition 45233 …, 2012 | 16 | 2012 |
| Overall effectiveness for a film cooled turbine blade leading edge with varying hole pitch TE Dyson, DG Bogard, JD Piggush, A Kohli Turbo Expo: Power for Land, Sea, and Air 43994, 1879-1887, 2010 | 15 | 2010 |
| Double impingement slot cap assembly TE Dyson, D Getsinger US Patent 10,577,942, 2020 | 14 | 2020 |
| Cooling assembly for a turbine assembly TE Dyson, DR Getsinger, NW Rathay US Patent App. 15/379,988, 2018 | 12 | 2018 |
| Engine component with hollow turbulators ER Clark, JR Winka, DR Getsinger, TE Dyson, BG Brzek, ... US Patent 10,577,944, 2020 | 11 | 2020 |
| Airfoil with tip rail cooling NW Rathay, TE Dyson, BJ Leary, GT Garay, GA Ledezma, DW Weber, ... US Patent 10,753,207, 2020 | 10 | 2020 |
| A CFD evaluation of multiple RANS turbulence models for prediction of boundary layer flows on a turbine vane TE Dyson, DG Bogard, SD Bradshaw Turbo Expo: Power for Land, Sea, and Air 55164, V03CT14A014, 2013 | 10 | 2013 |
