Nico De Tullio
Title
Cited by
Cited by
Year
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
121*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), 094105, 2010
332010
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, 2015
272015
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
172009
Direct numerical simulations of roughness receptivity and transitional shock-wave/boundary-layer interactions
N De Tullio, ND Sandham
RTO-MP-AVT-200. Art. 22, NATO, 2012
152012
Receptivity and transition to turbulence of supersonic boundary layers with surface roughness
N De Tullio
University of Southampton, 2013
122013
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
102019
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
102015
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
82018
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
52018
Transitional shock-wave/boundary layer interaction behind a roughness element
N De Tullio, ND Sandham
28th International Symposium on Shock Waves, 439-445, 2012
32012
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, 91-96, 2015
22015
Direct numerical simulations and modal analysis of subsonic flow over swept airfoil sections
N De Tullio, ND Sandham
arXiv preprint arXiv:1901.04727, 2019
12019
Transitional separation bubbles over swept wings
N De Tullio, ND Sandham
Tenth International Symposium on Turbulence and Shear Flow Phenomena, 2017
12017
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
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Articles 1–19