| Strut injectors for scramjets: Total pressure losses in two streamwise vortex interactions F Vergine, C Ground, L Maddalena Journal of Propulsion and Power 33 (5), 1140-1150, 2017 | 25 | 2017 |
| Turbulent kinetic energy decay in supersonic streamwise interacting vortices F Vergine, C Ground, L Maddalena Journal of Fluid Mechanics 807, 353-385, 2016 | 19 | 2016 |
| Filtered Rayleigh scattering mixing measurements of merging and non-merging streamwise vortex interactions in supersonic flow CR Ground, V Gopal, L Maddalena Experiments in Fluids 59, 1-17, 2018 | 13 | 2018 |
| Fast approximations of spectral lineshapes to enable optimization of a filtered Rayleigh scattering experiment GJ Hunt, CR Ground, RL Hunt Measurement Science and Technology 31 (9), 095203, 2020 | 11 | 2020 |
| The effect of vortex merging and non-merging on the transfer of modal turbulent kinetic energy content C Ground, F Vergine, L Maddalena Experiments in Fluids 57, 1-15, 2016 | 11 | 2016 |
| Computational analysis and characterization of the UTA 1.6 MW arc-heated wind tunnel facility C Ground, L Maddalena, V Viti 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2013 | 7 | 2013 |
| Teflon probing for the flow characterization of arc-heated wind tunnel facilities S Gulli, C Ground, M Crisanti, L Maddalena Experiments in fluids 55, 1-18, 2014 | 6 | 2014 |
| Simple, fast nitric oxide planar laser-induced fluorescence model for computational fluid dynamics applications TG Drozda, CR Ground, WT Knapp, PM Danehy AIAA Journal 61 (4), 1759-1771, 2023 | 5 | 2023 |
| Comparison of intrusive and non-intrusive mixture composition measurements in supersonic flow C Ground, D Viganó, L Maddalena Journal of Propulsion and Power 34 (6), 1574-1585, 2018 | 5 | 2018 |
| Analysis of the Two-Level NO PLIF Model for Low-Temperature High-Speed Flow Applications TG Drozda, CR Ground, AR Ziltz, KF Cabell, JA Inman, BF Bathel, ... 22nd AIAA International Space Planes and Hypersonics Systems and …, 2018 | 4 | 2018 |
| Visualization of supersonic turbulent vortical flows with filtered Rayleigh scattering C Ground, L Maddalena Journal of Visualization 20, 75-86, 2017 | 4 | 2017 |
| Design and application of filtered Rayleigh scattering experiments for mixing studies of new strut injectors for scramjets CR Ground, D Thumiah, L Maddalena 31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2567, 2015 | 4 | 2015 |
| Quantitative gas property measurements by filtered Rayleigh scattering: a review CR Ground, RL Hunt, GJ Hunt Measurement Science and Technology 34 (9), 092001, 2023 | 3 | 2023 |
| Comparison of several global mixing performance metrics for high-speed fuel injectors CR Ground, TG Drozda, KF Cabell, EL Axdahl 22nd AIAA international space planes and hypersonics systems and …, 2018 | 3 | 2018 |
| Computational study and error analysis of an integrated sampling-probe and gas-analyzer for mixing measurements in supersonic flow W Zhu, C Ground, L Maddalena, V Viti Measurement Science and Technology 27 (9), 095301, 2016 | 3 | 2016 |
| Design of a model scramjet combustor for vortex-enhanced mixing and combustion studies CR Ground, W Zhu, L Maddalena 19th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2014 | 3 | 2014 |
| Experimental and numerical investigation of the flow characteristics of a strut injector for scramjets CR Ground, F Vergine, L Maddalena, V Viti 19th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2014 | 3 | 2014 |
| Numerical analysis and characterization of the dissociated flowfield inside a 1.6 MW arc-heated wind tunnel facility C Ground, L Maddalena, V Viti Aerospace Science and Technology 30 (1), 306-314, 2013 | 3 | 2013 |
| Analytical and Experimental Demonstration of an Alternate Mixing Performance Metric for High-Speed Fuel Mixing Studies CR Ground, KF Cabell, TG Drozda AIAA AVIATION 2020 FORUM, 3106, 2020 | 2 | 2020 |
| Experimental study of strut injectors for scramjet combustors: Total pressure losses in a selected supersonic streamwise vortex interaction mode F Vergine, C Ground, L Maddalena 20th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2015 | 2 | 2015 |
Tomasz DrozdaNASAVerified email at nasa.gov
