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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: [email protected]

Collaborating research institutes, centres and groups

Research outputs

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
Comparison of three large-eddy simulations of shock-induced turbulent separation bubbles
Emile Touber & Neil D. Sandham, 2009, Shock Waves, 19(6), 469-478
DOI: 10.1007/s00193-009-0222-x
Type: article
Numerical study of mach 6 boundary-layer stabilization by means of a porous surface
N.D. Sandham & H. Ludeke, 2009, AIAA Journal, 47(9), 2243-2252
DOI: 10.2514/1.43388
Type: article
Shock-wave/boundary-layer interactions in a model scramjet intake
L. Krishnan, N.D. Sandham & J. Steelant, 2009, AIAA Journal, 47(7), 1680-1691
DOI: 10.2514/1.41107
Type: article