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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

Numerical simulation of transpiration cooling for a high-speed boundary layer undergoing transition to turbulence
Pushpender K. Sharma, Ralf Deiterding, Adriano Cerminara & Neil Sandham, 2023, Aerospace Science and Technology, 141
DOI: 10.1016/j.ast.2023.108581
Type: article
Development of an adaptive strand-Cartesian solver in 2D for non-equilibrium aerothermodynamics simulations
Chay William Charles Atkins & Ralf Deiterding, 2022
Type: conference
Transpiration cooling of hypersonic flow past a flat plate with porous injection
Pushpender Sharma, Ralf Deiterding & Neil Sandham, 2022
Type: conference
A two-dimensional parallel strand/CAMR solver for hypersonic flow simulations
Chay, William Charles Atkins & Ralf Deiterding, 2022
Type: conference
Transpiration cooling of hypersonic flow past a flat plate with porous injection
Pushpender Sharma, Ralf Deiterding & Neil Sandham, 2022
Type: conference
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