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Research project

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

Research groups:

Aerodynamics and Flight Mechanics Group
Lead researcher:

Professor Neil Sandham
Research funder:

EPSRC
Status:

Not active

Staff

Lead researcher

Professor Neil Sandham

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

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