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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

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