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Research project

Sandham - Next generation of SBLI code, EP/F011016/1

Research groups:

Aerodynamics and Flight Mechanics Group
Lead researchers:

Professor Neil Sandham
Research funder:

EPSRC
Status:

Not active

Staff

Lead researchers

Professor Neil Sandham

Professor Neil Sandham

Professor of Aerospace Engineering

Research interests

Transonic aerodynamics of wings
Hypersonic flows with transition to turbulence
Flow over rough surfaces

Connect with Neil

Email: n.sandham@soton.ac.uk

Collaborating research institutes, centres and groups

Aerodynamics and Flight Mechanics Group

Our group undertakes research on fundamental fluid dynamics, applied aerodynamics, flow control, flight dynamics and aeroacoustics.

Research outputs

Transitional shock-wave/boundary-layer interactions in hypersonic flow

N.D. Sandham, E. Schuelein, A Wagner, S Willems & J Steelant, 2014, Journal of Fluid Mechanics, 752, 1-33

DOI: 10.1017/jfm.2014.333

Type: article

Laminar-turbulent transition induced by a discrete roughness element in a supersonic boundary layer

N. De Tullio, P. Paredes, N. D. Sandham & V. Theofilis, 2013, Journal of Fluid Mechanics, 735, 613-646

DOI: 10.1017/jfm.2013.520

Type: article

Numerical simulations of turbulent spots in supersonic boundary layers: effects of Mach number and wall temperature

J.A. Redford, N.D. Sandham & G.T. Roberts, 2012, Progress in Aerospace Sciences, 52, 67-79

DOI: 10.1016/j.paerosci.2011.08.002

Type: article

Low-order stochastic modelling of low-frequency motions in reflected shock-wave/boundary-layer interactions

Emile Touber & Neil D. Sandham, 2011, Journal of Fluid Mechanics, 671, 417-465

DOI: 10.1017/S0022112010005811

Type: article

Compressibility effects on boundary layer transition induced by an isolated roughness element

J.A. Redford, N.D. Sandham & G.T. Roberts, 2010, AIAA Journal, 48(12), 2818-2830

DOI: 10.2514/1.J050186

Type: article

Direct numerical simulation of transitional flow at high Mach number coupled with a wall heating model

J.A. Redford, N.D. Sandham & G.T. Roberts, 2010, Computers & Fluids, 45, 37-46

DOI: 10.1016/j.compfluid.2010.11.024

Type: article

Direct numerical simulation of breakdown to turbulence in a Mach 6 boundary layer over a porous surface

Nicola De Tullio & Neil D. Sandham, 2010, Physics of Fluids, 22, 094105- [15pp]

DOI: 10.1063/1.3481147

Type: article