| Laminar–turbulent transition induced by a discrete roughness element in a supersonic boundary layer N De Tullio, P Paredes, ND Sandham, V Theofilis Journal of Fluid Mechanics 735, 613 - 643, 2013 | 178* | 2013 |
| Direct numerical simulation of breakdown to turbulence in a Mach 6 boundary layer over a porous surface N De Tullio, ND Sandham Physics of Fluids 22 (9), 2010 | 60 | 2010 |
| Influence of boundary-layer disturbances on the instability of a roughness wake in a high-speed boundary layer N De Tullio, ND Sandham Journal of Fluid Mechanics 763, 136-165, 2015 | 43 | 2015 |
| Direct numerical simulations of transonic flow around an airfoil at moderate Reynolds numbers M Zauner, N De Tullio, ND Sandham AIAA Journal 57 (2), 597-607, 2019 | 38 | 2019 |
| A numerical evaluation of the asymptotic theory of receptivity for subsonic compressible boundary layers N De Tullio, AI Ruban Journal of Fluid Mechanics 771, 520-546, 2015 | 26 | 2015 |
| Re-engineering a DNS code for high-performance computation of turbulent flows Y Yao, Z Shang, J Castagna 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and …, 2009 | 20 | 2009 |
| Direct numerical simulations of roughness receptivity and transitional shock-wave/boundary-layer interactions N De Tullio, ND Sandham NATO RTO AVT-200 Specialists Meeting on Hypersonic Laminar-Turbulent …, 2012 | 18 | 2012 |
| An error indicator for finite difference methods using spectral techniques with application to aerofoil simulation CT Jacobs, M Zauner, N De Tullio, SP Jammy, DJ Lusher, ND Sandham Computers & Fluids 168, 67-72, 2018 | 16 | 2018 |
| Receptivity and transition to turbulence of supersonic boundary layers with surface roughness N De Tullio University of Southampton, 2013 | 16 | 2013 |
| Instability study of the wake behind a discrete roughness element in a hypersonic boundary-layer P Paredes, N De Tullio, ND Sandham, V Theofilis Instability and Control of Massively Separated Flows: Proceedings of the …, 2015 | 6 | 2015 |
| Direct numerical simulations and modal analysis of subsonic flow over swept airfoil sections N De Tullio, ND Sandham arXiv preprint arXiv:1901.04727, 2019 | 5 | 2019 |
| Unsteady behaviour in direct numerical solutions of transonic flow around an airfoil. M Zauner, N De Tullio, N Sandham 2018 Fluid Dynamics Conference, 2911, 2018 | 4 | 2018 |
| Transitional shock-wave/boundary layer interaction behind a roughness element N De Tullio, ND Sandham 28th International Symposium on Shock Waves: Vol 2, 439-445, 2012 | 3 | 2012 |
| Transitional separation bubbles over swept wings N De Tullio, ND Sandham Tenth International Symposium on Turbulence and Shear Flow Phenomena, 2017 | 1 | 2017 |
| Global Stability Analysis and DNS of a Swept Airfoil Section in Subsonic Flow N De Tullio, ND Sandham IUTAM Laminar-Turbulent Transition: 9th IUTAM Symposium, London, UK …, 2021 | | 2021 |
| Performance analysis of a heaving wing using DNS and LES N De Tullio, Z Xie, J Chalke, ND Sandham Direct and Large-Eddy Simulation XI, 397-403, 2019 | | 2019 |
| Dataset for direct numerical simulations of a transonic airfoil at a Reynolds number of Re= 500,000 M Zauner, N Sandham, N De Tullio University of Southampton, 2018 | | 2018 |
| Error severity values from simulations of a Taylor-Green vortex and a V2C aerofoil, computed using an error indicator CT Jacobs, M Zauner, N De Tullio, S Jammy, D Lusher, N Sandham University of Southampton, 2018 | | 2018 |
| Assessment of the asymptotic theory of receptivity using numerical simulations of the compressible Navier-Stokes equations N De Tullio, A Ruban 10th European Fluid Mechanics Conference, 2014 | | 2014 |
| ExaFLOW use case for SBLI: numerical simulation of the compressible flow over a NACA-4412 airfoil at incidence N De Tullio, ND Sandham | | |
Neil D. SandhamProfessor, University of Southampton在 soton.ac.uk 的电子邮件经过验证
