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Research project

Transpiration Cooling Systems for Jet Engine Turbines and Hypersonic Flight

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

Other researchers

Professor Ralf Deiterding

Professor
Connect with Ralf

Email: R.Deiterding@soton.ac.uk

Collaborating research institutes, centres and groups

Research outputs

Influence of instability modes on cooling performance in hypersonic boundary layer with slot injection
Adriano Cerminara, Tobias Hermann, Hassan Saad Ifti, Ralf Deiterding, Neil Sandham & Matthew McGilvray, 2021, Aerospace Science and Technology, 109
DOI: 10.1016/j.ast.2020.106409
Type: article
A mesoscopic modelling approach for direct numerical simulations of transition to turbulence in hypersonic flow with transpiration cooling
Adriano Cerminara, Ralf Deiterding & Neil Sandham, 2020, International Journal of Heat and Fluid Flow, 86
DOI: 10.1016/j.ijheatfluidflow.2020.108732
Type: article
Towards a strand/Cartesian AMR solver for modelling hypersonic flows in thermochemical nonequilibrium
Chay, William Charles Atkins & Ralf Deiterding, 2020
DOI: 10.2514/6.2020-2404
Type: conference
Transpiration cooling using porous material for hypersonic applications
Adriano Cerminara, Ralf Deiterding & Neil Sandham, 2019
Type: bookChapter
Direct numerical simulations of coolant injection through a porous layer for transpiration cooling in hypersonic flow
Adriano Cerminara, Ralf Deiterding & Neil Sandham, 2019
Type: report