Transpiration cooling for double-walled jet engine turbine blades by Courtis, M

Multiscale analysis of thermomechanical stresses in double wall transpiration cooling systems for gas turbine blades by Skamniotis, C, Courtis, M, Cocks, ACF

Coupled aerothermal-mechanical analysis in single crystal double wall transpiration cooled gas turbine blades with a large film hole density by Courtis, M, Skamniotis, C, Cocks, A, Ireland, P

Influence of spanwise and streamwise film hole spacing on adiabatic film effectiveness for effusion-cooled gas turbine blades by Courtis, M, Murray, A, Coulton, B, Ireland, P, Mayo, I