Non-intrusive measurement techniques for flow characterization of hypersonic wind tunnels PM Danehy, J Weisberger, C Johansen, D Reese, T Fahringer, ... STO-VKI-LS on" Flow Characterization and Modeling of Hypersonic Wind Tunnels", 2018 | 52 | 2018 |
Simultaneous direct measurements of concentration and velocity in the Richtmyer–Meshkov instability DT Reese, AM Ames, CD Noble, JG Oakley, DA Rothamer, R Bonazza Journal of Fluid Mechanics 849, 541-575, 2018 | 38 | 2018 |
FLEET velocimetry for aerodynamics PM Danehy, RA Burns, DT Reese, JE Retter, SP Kearney Annual Review of Fluid Mechanics 54 (1), 525-553, 2022 | 26 | 2022 |
Application of femtosecond-laser tagging for unseeded velocimetry in a large-scale transonic cryogenic wind tunnel DT Reese, RJ Thompson, RA Burns, PM Danehy Experiments in Fluids 62, 1-19, 2021 | 14 | 2021 |
Application of resonant femtosecond tagging velocimetry in the 0.3-meter transonic cryogenic tunnel D Reese, P Danehy, N Jiang, J Felver, D Richardson, J Gord AIAA Journal 57 (9), 3851-3858, 2019 | 14 | 2019 |
A cryogenic RE oscillator, the heart of a new NMR dispersion spectrometer B Van Riet, L Van Gerven Journal of Physics E: Scientific Instruments 15 (5), 558, 1982 | 12 | 1982 |
Unseeded velocimetry in nitrogen for high-pressure, cryogenic wind tunnels: part III. Resonant femtosecond-laser tagging DT Reese, N Jiang, P Danehy Measurement Science and Technology 31 (7), 075203, 2020 | 11 | 2020 |
Simultaneous concentration and velocity field measurements in a shock-accelerated mixing layer D Reese, J Oakley, A Navarro-Nunez, D Rothamer, C Weber, R Bonazza Experiments in fluids 55, 1-8, 2014 | 11 | 2014 |
Implementation of a pulsed-laser measurement system in the National Transonic Facility D Reese, RA Burns, PM Danehy, E Walker, W Goad AIAA Aviation 2019 Forum, 3380, 2019 | 9 | 2019 |
FLEET velocimetry in the common research model’s wing wake D Reese, PM Danehy, EL Walker, MB Rivers, WK Goad AIAA Scitech 2020 Forum, 1276, 2020 | 8 | 2020 |
Numerical investigation of 3D effects on a 2D-dominated shocked mixing layer D Reese, C Weber Physics of Fluids 28 (11), 2016 | 8 | 2016 |
On the use of liquid nitrogen droplets as flow tracers in cryogenic flow facilities at NASA Langley Research Center JE Retter, RA Burns, J Fisher, J Felver, D Reese, PM Danehy AIAA Scitech 2021 Forum, 1301, 2021 | 5 | 2021 |
Application of STARFLEET velocimetry in the NASA Langley 0.3-meter transonic cryogenic tunnel D Reese, PM Danehy, N Jiang, J Felver, DR Richardson, JR Gord 2018 aerodynamic measurement technology and ground testing conference, 2989, 2018 | 5 | 2018 |
Implementation of an Unsteady PSP System in the NASA Transonic Dynamics Tunnel D Reese, S Peak, K Goodman, N Watkins AIAA AVIATION 2022 Forum, 3784, 2022 | 2 | 2022 |
Direct Measurements of Concentration and Velocity in the Richtmyer-Meshkov Instability DT Reese University of Wisconsin--Madison, 2017 | 1 | 2017 |
Improvement of Pressure Sensitive Paint in A Cryogenic Oxygen-Poor Environment AN Watkins, D Reese | | 2023 |
Advances in PSP Testing in LaRC High Reynolds Number Facilities DT Reese, AN Watkins AIAA SciTech Forum, 2023 | | 2023 |
Single-Component Average Velocity Profiles in the Wake of the Orion Crew Capsule at the National Transonic Facility JE Retter, OK Tyrrell, B Moran, J Montgomery, W Dressler, KL Bibb, ... AIAA SCITECH 2023 Forum, 2259, 2023 | | 2023 |
Implementation of an Unsteady PSP System in the NASA TDT D Reese, S Peak, K Goodman, N Watkins Aviation Forum, 2022 | | 2022 |
Off-Body Velocimetry in Transonic Cryogenic Ground Test Facilities at NASA Langley Research Center J Retter, D Reese, P Danehy North Carolina State University Seminar, 2020 | | 2020 |