| Development of the US3D code for advanced compressible and reacting flow simulations GV Candler, HB Johnson, I Nompelis, VM Gidzak, PK Subbareddy, ... 53rd AIAA Aerospace Sciences Meeting, 1893, 2015 | 270 | 2015 |
| 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 | 222 | 2015 |
| Development of a hybrid unstructured implicit solver for the simulation of reacting flows over complex geometries I Nompelis, T Drayna, G Candler 34th AIAA Fluid Dynamics Conference and Exhibit, 2227, 2004 | 220 | 2004 |
| A parallel unstructured implicit solver for hypersonic reacting flow simulation I Nompelis, TW Drayna, GV Candler Parallel Computational Fluid Dynamics 2005, 389-395, 2006 | 202 | 2006 |
| Effect of vibrational nonequilibrium on hypersonic double-cone experiments I Nompelis, GV Candler, MS Holden AIAA journal 41 (11), 2162-2169, 2003 | 171 | 2003 |
| Effects of numerics on Navier-Stokes computations of hypersonic double-cone flows MC Druguet, GV Candler, I Nompelis AIAA journal 43 (3), 616-623, 2005 | 154 | 2005 |
| Assessment of CFD capability for prediction of hypersonic shock interactions D Knight, J Longo, D Drikakis, D Gaitonde, A Lani, I Nompelis, B Reimann, ... Progress in Aerospace Sciences 48, 8-26, 2012 | 152 | 2012 |
| FIRE II calculations for hypersonic nonequilibrium aerothermodynamics code verification: DPLR, LAURA, and US3D D Hash, J Olejniczak, M Wright, D Prabhu, M Pulsonetti, B Hollis, P Gnoffo, ... 45th AIAA Aerospace Sciences Meeting and Exhibit, 605, 2007 | 141 | 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 | 131 | 2015 |
| CFD validation for hypersonic flight-Hypersonic double-cone flow simulations G Candler, I Nompelis, MC Druguet, M Holden, T Wadhams, I Boyd, ... 40th AIAA aerospace sciences meeting & exhibit, 581, 2002 | 128 | 2002 |
| Unstructured grid approaches for accurate aeroheating simulations G Candler, M Barnhardt, T Drayna, I Nompelis, D Peterson, P Subbareddy 18th AIAA computational fluid dynamics conference, 3959, 2007 | 105 | 2007 |
| Assessment of predictive capabilities for aerodynamic heating in hypersonic flow D Knight, O Chazot, J Austin, MA Badr, G Candler, B Celik, D de Rosa, ... Progress in Aerospace Sciences 90, 39-53, 2017 | 101 | 2017 |
| Computational study of hypersonic double-cone experiments for code validation I Nompelis University of Minnesota, 2004 | 87 | 2004 |
| Hypersonic inward turning inlets: design and optimization T Drayna, I Nompelis, G Candler 44th AIAA Aerospace Sciences Meeting and Exhibit, 297, 2006 | 82 | 2006 |
| Navier-Stokes predictions of hypersonic double-cone and cylinder-flare flow fields G Candler, I Nompelis, MC Druguet 39th Aerospace Sciences Meeting and Exhibit, 1024, 2001 | 66 | 2001 |
| Nonequilibrium flow through porous thermal protection materials, Part I: Numerical methods EC Stern, S Poovathingal, I Nompelis, TE Schwartzentruber, GV Candler Journal of Computational Physics 380, 408-426, 2019 | 58 | 2019 |
| Nonequilibrium flow through porous thermal protection materials, Part II: Oxidation and pyrolysis S Poovathingal, EC Stern, I Nompelis, TE Schwartzentruber, GV Candler Journal of Computational Physics 380, 427-441, 2019 | 51 | 2019 |
| Computational fluid dynamics for atmospheric entry GV Candler, I Nompelis Non-Equilibrium Dynamics: From Physical Models to Hypersonic Flights; The …, 2009 | 47 | 2009 |
| Decoupled implicit method for aerothermodynamics and reacting flows GV Candler, PK Subbareddy, I Nompelis AIAA journal 51 (5), 1245-1254, 2013 | 46 | 2013 |
| Detached eddy simulations of the MSL parachute at supersonic conditions M Barnhardt, T Drayna, I Nompelis, G Candler, W Garrard 19th AIAA aerodynamic decelerator systems technology conference and seminar …, 2007 | 45 | 2007 |
Graham V. CandlerRussell J. Penrose and McKnight Presidential Professor of Aerospace Engineering & MechanicsAdresă de e-mail confirmată pe umn.edu
