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Research project

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

Staff

Lead researcher

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
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
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, 2010, Progress in Aerospace Sciences, 52, 67-79
DOI: 10.1016/j.paerosci.2011.08.002
Type: article