| Nonequilibrium Gas Dynamics and Molecular Simulation ID Boyd, TE Schwartzentruber Cambridge University Press 1, 360, 2017 | 342 | 2017 |
| An improved potential energy surface and multi-temperature quasiclassical trajectory calculations of N2+ N2 dissociation reactions JD Bender, P Valentini, I Nompelis, Y Paukku, Z Varga, DG Truhlar, ... The Journal of chemical physics 143 (5), 2015 | 242 | 2015 |
| A hybrid particle-continuum method applied to shock waves TE Schwartzentruber, ID Boyd Journal of Computational Physics 215 (2), 402-416, 2006 | 222 | 2006 |
| A modular particle–continuum numerical method for hypersonic non-equilibrium gas flows TE Schwartzentruber, LC Scalabrin, ID Boyd Journal of Computational Physics 225 (1), 1159-1174, 2007 | 198 | 2007 |
| Direct molecular simulation of nitrogen dissociation based on an ab initio potential energy surface P Valentini, TE Schwartzentruber, JD Bender, I Nompelis, GV Candler Physics of Fluids 27 (8), 2015 | 150 | 2015 |
| Determination of the scalar friction factor for nonspherical particles and aggregates across the entire Knudsen number range by direct simulation Monte Carlo (DSMC) C Zhang, T Thajudeen, C Larriba, TE Schwartzentruber, CJ Hogan Jr Aerosol Science and Technology 46 (10), 1065-1078, 2012 | 143 | 2012 |
| Oxygen interactions with silica surfaces: Coupled cluster and density functional investigation and the development of a new ReaxFF potential AD Kulkarni, DG Truhlar, S Goverapet Srinivasan, ACT Van Duin, ... The Journal of Physical Chemistry C 117 (1), 258-269, 2013 | 139 | 2013 |
| Direct molecular simulation of nonequilibrium dilute gases TE Schwartzentruber, MS Grover, P Valentini Journal of Thermophysics and Heat Transfer 32 (4), 892-903, 2018 | 120 | 2018 |
| Air–carbon ablation model for hypersonic flight from molecular-beam data KS Prata, TE Schwartzentruber, TK Minton AIAA journal 60 (2), 627-640, 2022 | 112 | 2022 |
| Direct molecular simulation of internal energy relaxation and dissociation in oxygen MS Grover, E Torres, TE Schwartzentruber Physics of Fluids 31 (7), 2019 | 111 | 2019 |
| Hybrid particle-continuum simulations of nonequilibrium hypersonic blunt-body flowfields TE Schwartzentruber, LC Scalabrin, ID Boyd Journal of Thermophysics and Heat Transfer 22 (1), 29-37, 2008 | 109 | 2008 |
| Dynamics of nitrogen dissociation from direct molecular simulation P Valentini, TE Schwartzentruber, JD Bender, GV Candler Physical Review Fluids 1 (4), 043402, 2016 | 102 | 2016 |
| Implementation of a chemical kinetics model for hypersonic flows in air for high-performance CFD RS Chaudhry, ID Boyd, E Torres, TE Schwartzentruber, GV Candler AIAA Scitech 2020 Forum, 2191, 2020 | 101 | 2020 |
| Construction of a coarse-grain quasi-classical trajectory method. II. Comparison against the direct molecular simulation method RL Macdonald, MS Grover, TE Schwartzentruber, M Panesi The Journal of chemical physics 148 (5), 2018 | 101 | 2018 |
| Finite-rate oxidation model for carbon surfaces from molecular beam experiments S Poovathingal, TE Schwartzentruber, VJ Murray, TK Minton, GV Candler AIAA journal 55 (5), 1644-1658, 2017 | 99 | 2017 |
| Vibrational Energy Transfer and Collision-Induced Dissociation in Collisions MS Grover, TE Schwartzentruber, Z Varga, DG Truhlar Journal of Thermophysics and Heat Transfer 33 (3), 797-807, 2019 | 83 | 2019 |
| Molecular dynamics simulation of rotational relaxation in nitrogen: Implications for rotational collision number models P Valentini, C Zhang, TE Schwartzentruber Physics of Fluids 24 (10), 2012 | 76 | 2012 |
| General drag coefficient for flow over spherical particles N Singh, M Kroells, C Li, E Ching, M Ihme, CJ Hogan, ... AIAA journal 60 (2), 587-597, 2022 | 73 | 2022 |
| GPU-accelerated classical trajectory calculation direct simulation Monte Carlo applied to shock waves P Norman, P Valentini, T Schwartzentruber Journal of Computational Physics 247, 153-167, 2013 | 71 | 2013 |
| Robust cut-cell algorithms for DSMC implementations employing multi-level Cartesian grids C Zhang, TE Schwartzentruber Computers & fluids 69, 122-135, 2012 | 70 | 2012 |
Graham V. CandlerRussell J. Penrose and McKnight Presidential Professor of Aerospace Engineering & MechanicsVerified email at umn.edu
