| Blackout analysis of Mars entry missions S Ramjatan, A Lani, S Boccelli, B Van Hove, Ö Karatekin, T Magin, ... Journal of Fluid Mechanics 904 (A26), 37, 2020 | 30 | 2020 |
| Blackout Analysis of Small Cone-Shaped Reentry Vehicles S Ramjatan, T Magin, T Scholz, V Van der Haegen, J Thoemel Journal of Thermophysics and Heat Transfer 31 (2), 269-282, 2017 | 14 | 2017 |
| Micro-Scale Thermal-Structural Modeling for Carbon Fibers R Fu, S Ramjatan, M Kroells, T Schwartzentruber, A Martin AIAA AVIATION 2020 FORUM, 3273, 2020 | 5 | 2020 |
| Dsmc simulation of ablating microstructures at flight relevant conditions S Ramjatan, MD Kroells, TE Schwartzentruber AIAA Scitech 2021 Forum, 1052, 2021 | 4 | 2021 |
| Magnus effect on a spinning satellite in low earth orbit S Ramjatan, N Fitz-Coy, A Yew AIAA/AAS Astrodynamics Specialist Conference, 5257, 2016 | 4 | 2016 |
| Surface Properties on Thermal Protection System Microstructure during Hypersonic Ablation AD Achambath, S Ramjatan, TE Schwartzentruber AIAA Scitech 2019 Forum, 1283, 2019 | 3 | 2019 |
| Blackout analysis of small reentry vehicles S Ramjatan, TE Magin, T Scholz, V Van der Haegen, J Thoemel 53rd AIAA Aerospace Sciences Meeting, 2081, 2015 | 3 | 2015 |
| Effect of blowing mass flux on porous mesostructure surface properties for hypersonic ablation S Ramjatan, MD Kroells, TE Schwartzentruber AIAA SCITECH 2022 Forum, 1644, 2022 | 1 | 2022 |
| Aerothermal Loads on a Representative Porous Mesostructure at Flight Conditions Using Direct Simulation Monte Carlo M Kroells, S Ramjatan, TE Schwartzentruber Journal of Thermophysics and Heat Transfer 38 (4), 491-507, 2024 | | 2024 |
| Microscale Thermal–Structural Modeling for Carbon Fibers Subjected to a Hypersonic Boundary Layer R Fu, A Martin, S Ramjatan, M Kroells, TE Schwartzentruber Journal of Spacecraft and Rockets, 1-11, 2024 | | 2024 |
| Air-carbon ablation resulting from boundary layer flow over resolved material microstructure S Ramjatan, J Douglas, TE Schwartzentruber AIAA AVIATION 2023 Forum, 3326, 2023 | | 2023 |
Tom SchwartzentruberProfessor of Aerospace Engineering and Mechanics, University of Minnesota在 aem.umn.edu 的电子邮件经过验证
