| Experimental study of rotating detonation combustor performance under preheat and back pressure operation A Roy, DH Ferguson, T Sidwell, B O'Meara, P Strakey, C Bedick, A Sisler 55th AIAA aerospace sciences meeting, 1065, 2017 | 75 | 2017 |
| A novel transient technique to determine recovery temperature, heat transfer coefficient, and film cooling effectiveness simultaneously in a transonic turbine cascade S Xue, A Roy, WF Ng, SV Ekkad Journal of Thermal Science and Engineering Applications 7 (1), 011016, 2015 | 70 | 2015 |
| Heat Transfer Performance of a Transonic Turbine Blade Passage in the Presence of Leakage Flow Through Upstream Slot and Mateface Gap With Endwall Contouring A Roy, S Jain, SV Ekkad, W Ng, AS Lohaus, ME Crawford, S Abraham Journal of Turbomachinery 139 (12), 121006, 2017 | 54 | 2017 |
| Heat transfer coefficients of additively manufactured tubes with internal pin fins for supercritical carbon dioxide cycle recuperators M Searle, J Black, D Straub, E Robey, J Yip, S Ramesh, A Roy, AS Sabau, ... Applied Thermal Engineering 181, 116030, 2020 | 31 | 2020 |
| Investigating instabilities in a rotating detonation combustor operating with natural gas–hydrogen fuel blend—effect of air preheat and annulus width A Roy, CR Bedick, DH Ferguson, T Sidwell, PA Strakey Journal of Engineering for Gas Turbines and Power 141 (11), 111017, 2019 | 29 | 2019 |
| Heat transfer performance of a transonic turbine blade passage in the presence of leakage flow through upstream slot and mateface gap with endwall contouring A Roy, S Jain, SV Ekkad, W Ng, AS Lohaus, ME Crawford, S Abraham Journal of Turbomachinery 139 (12), 121006, 2017 | 28 | 2017 |
| Experimental measurements of NOx emissions in a Rotating Detonation Engine DH Ferguson, B O'Meara, A Roy, K Johnson AIAA scitech 2020 forum, 0204, 2020 | 22 | 2020 |
| Unsteady heat transfer analysis to predict combustor wall temperature in rotating detonation engine A Roy, P Strakey, T Sidwell, DH Ferguson 51st AIAA/SAE/ASEE joint propulsion conference, 4191, 2015 | 22 | 2015 |
| Development of a three-dimensional transient wall heat transfer model of a rotating detonation combustor A Roy, P Strakey, T Sidwell, D Ferguson, A Sisler, A Nix 54th AIAA Aerospace Sciences Meeting, 0902, 2016 | 21 | 2016 |
| Effect of Upstream Purge Slot on a Transonic Turbine Blade Passage: Part 2—Heat Transfer Performance A Roy, DM Blot, SV Ekkad, WF Ng, AS Lohaus, ME Crawford Turbo Expo: Power for Land, Sea, and Air 55157, V03BT13A021, 2013 | 20 | 2013 |
| Measurement of Convective Heat Transfer Coefficients With Supercritical CO2 Using the Wilson-Plot Technique J Black, D Straub, E Robey, J Yip, S Ramesh, A Roy, M Searle Journal of energy resources technology 142 (7), 070901, 2020 | 17 | 2020 |
| Effect of endwall contouring on a transonic turbine blade passage: heat transfer performance KV Panchal, S Abraham, A Roy, SV Ekkad, W Ng, AS Lohaus, ... Journal of Turbomachinery 139 (1), 011009, 2017 | 17 | 2017 |
| Pressure Gain Combustion for Land Based Power Generation D Ferguson University Turbine Systems Research Confrence, 6-7, 2015 | 16 | 2015 |
| Aerodynamic performance of a transonic turbine blade passage in presence of upstream slot and mateface gap with endwall contouring S Jain, A Roy, W Ng, S Ekkad, AS Lohaus, F Taremi Turbo Expo: Power for Land, Sea, and Air 45622, V02CT38A036, 2014 | 13 | 2014 |
| Thermal management of a transonic turbine: leakage flow and endwall contouring effects A Roy, DM Blot, SV Ekkad, WF Ng, AS Lohaus, ME Crawford, S Abraham Journal of Thermophysics and Heat Transfer 32 (4), 1031-1044, 2018 | 11 | 2018 |
| A physics based reactor network model of a rotating detonation engine combustor A Roy, D Ferguson Turbo Expo: Power for Land, Sea, and Air 56697, V04BT04A065, 2015 | 11 | 2015 |
| Investigating Gas Turbine Internal Cooling Using Supercritical CO2 at Higher Reynolds Numbers for Direct Fired Cycle Applications M Searle, A Roy, J Black, D Straub, S Ramesh Journal of Turbomachinery 144 (1), 011007, 2022 | 8 | 2022 |
| Investigating Gas Turbine Internal Cooling Using Supercritical CO2 at High Reynolds Numbers for Direct Fired Cycle Applications M Searle, A Roy, J Black, D Straub, S Ramesh Turbo Expo: Power for Land, Sea, and Air 85048, V010T30A020, 2021 | 7 | 2021 |
| Characteristics of a Non-Premixed Rotating Detonation Combustor Using Natural Gas-Hydrogen Blend at Elevated Air-Preheat Temperature and Backpressure A Roy, D Ferguson, T Sidwell, P Strakey ASME International Mechanical Engineering Congress and Exposition 52118 …, 2018 | 7 | 2018 |
| Effect of Upstream Purge Slot on a Transonic Turbine Blade Passage: Part 1—Aerodynamic Performance DM Blot, A Roy, SV Ekkad, W Ng, AS Lohaus, ME Crawford Turbo Expo: Power for Land, Sea, and Air 55157, V03BT13A023, 2013 | 6 | 2013 |
Doug StraubNational Energy Technology LaboratoryVerified email at netl.doe.gov
