Open menu
View all research projects
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

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

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
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
Large-eddy simulation of low-frequency unsteadiness in a turbulent shock-induced separation bubble
Emile Touber,
& Neil D. Sandham
, 2009 , Theoretical and Computational Fluid Dynamics , 23 (2) , 79--107
DOI: 10.1007/s00162-009-0103-z
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