| Experimental testing of an RP-2-GOX rotating detonation rocket engine D Lim, J Humble, SD Heister AIAA Scitech 2020 Forum, 0195, 2020 | 27 | 2020 |
| Transient response of a liquid injector to a steep-fronted transverse pressure wave D Lim, S Heister, D Stechmann, B Kan Shock Waves 28, 919-932, 2018 | 17 | 2018 |
| Experimental investigation of wall heat flux in a rotating detonation rocket engine D Lim, SD Heister, J Humble, AJ Harroun Journal of Spacecraft and Rockets 58 (5), 1444-1452, 2021 | 16 | 2021 |
| Experimental Studies of Liquid Injector Response and Wall Heat Flux in a Rotating Detonation Rocket Engine D Lim Purdue University, 2019 | 12 | 2019 |
| Response of angled and tapered liquid injectors to passing detonation fronts at high operating pressures HF Celebi, D Lim, KJ Dille, SD Heister Shock Waves 31 (7), 717-726, 2021 | 8 | 2021 |
| Transient response of a liquid injector to a transverse detonation wave at elevated initial pressure D Lim, SD Heister 2018 AIAA Aerospace Sciences Meeting, 0632, 2018 | 7 | 2018 |
| Transient response of a liquid injector to a transverse pressure wave D Lim, SD Heister, DP Stechmann, B Kan, B Justice 51st AIAA/SAE/ASEE Joint Propulsion Conference, 3767, 2015 | 6 | 2015 |
| Transient response of a liquid injector to an ethylene-oxygen detonation wave D Lim, HF Celebi, SD Heister AIAA SciTech 2019 Forum, 1513, 2019 | 5 | 2019 |
| Experimental study of liquid injector elements for use in rotating detonation engines W Anderson, D Lim, SD Heister 55th AIAA Aerospace Sciences Meeting, 1932, 2017 | 4 | 2017 |
| Design and Analysis of a High-Performance Hydrogen Peroxide Thrust Chamber Assembly DP Stechmann, D Lim, S Rotella, S Menon, B Nirudhoddi 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 3500, 2014 | 2 | 2014 |
| Experimental Study of a High Pressure Rotating Detonation Wave Combustor for Rocket Applications S Heister, D Stechmann, D Lim | | |
