| OH* chemiluminescence imaging of the combustion products from a methane-fueled rotating detonation engine J Tobias, D Depperschmidt, C Welch, R Miller, M Uddi, AK Agrawal, ... Journal of Engineering for Gas Turbines and Power 141 (2), 021021, 2019 | 48 | 2019 |
| Time-resolved PIV diagnostics to measure flow field exiting methane-fueled rotating detonation combustor D Depperschmidt, R Miller, J Tobias, M Uddi, AK Agrawal, JB Stout AIAA Scitech 2019 Forum, 1514, 2019 | 32 | 2019 |
| Experimental analysis of wave propagation in a methane-fueled rotating detonation combustor C Welch, D Depperschmidt, R Miller, J Tobias, M Uddi, AK Agrawal, ... Turbo Expo: Power for Land, Sea, and Air 51067, V04BT04A065, 2018 | 32 | 2018 |
| Rainbow schlieren imaging of density field in the exhaust flow of rotating detonation combustion R Miller, J Tobias, D Depperschmidt, K Bell, D Langner, AK Agrawal AIAA Propulsion and Energy 2019 Forum, 4380, 2019 | 16 | 2019 |
| Experimental and Computational Analysis of a Rotating Detonation Combustor J Tobias, AK Agrawal, DE Paxson AIAA SciTech 2022 Forum, 1879, 2022 | 13 | 2022 |
| Flow Measurements Inside a Rotating Detonation Combustor J Tobias, R Miller, AK Agrawal AIAA Propulsion and Energy 2020 Forum, 3869, 2020 | 13 | 2020 |
| Flow Development in Radial Plane of Rotating Detonation Engine Integrated with Aerospike JR Tobias, AK Agrawal Journal of Propulsion and Power 39 (3), 318-330, 2023 | 11 | 2023 |
| Uddi., M., Agrawal, AK, Stout, JB, Time-Resolved PIV Diagnostics to Measure Flow Field Exiting Methane-Fueled Rotating Detonation Combustor D Depperschmidt, J Tobias, R Miller AIAA-2019-1514, Presented at AIAA SciTech Forum 2019, San Diego, California, 2019 | 7 | 2019 |
| Time-resolved PIV measurements of flow field at the exit of a diffuser mounted on a rotating detonation combustor D Depperschmidt, J Tobias, R Miller, AK Agrawal AIAA Propulsion and Energy 2019 Forum, 4379, 2019 | 6 | 2019 |
| Time Resolved Flow Field in the Radial Plane of an Aerospike Integrated with a Rotating Detonation Combustor J Tobias, AK Agrawal AIAA Propulsion and Energy 2021 Forum, 3675, 2021 | 5 | 2021 |
| Effect of a Diffuser on Conditioning Flow Field Fluctuations at the Exit of a Rotating Detonation Combustor J Tobias, D Depperschmidt, R Miller, M Uddi, AK Agrawal Aerojet Rocketdyne, Sacramento, CA (United States), 2019 | 1 | 2019 |
| Time-Resolved PIV Measurements of Flow Field at Diffuser Exit Downstream of a Rotating Detonation Combustor DL Depperschmidt, JR Tobias, RS Miller, AK Agrawal Aerojet Rocketdyne, Sacramento, CA (United States), 2019 | | 2019 |
| Flow Measurements of Methane-Fueled Rotating Detonation Combustion D Depperschmidt, J Tobias, R Miller, M Uddi, A Agrawal, J Stout Aerojet Rocketdyne, Sacramento, CA (United States), 2018 | | 2018 |
| Exit Flow Field of Methane-Fueld Rotating Detonation Engine Measured by Time Resolved Particle Image Velocimetry D Depperschmidt, J Tobias, R Miller, M Uddi, A Agrawal Aerojet Rocketdyne, Sacramento, CA (United States), 2018 | | 2018 |
