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Research project

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

Staff

Lead researchers

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

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