| A converging slot-hole film-cooling geometry—part 1: low-speed flat-plate heat transfer and loss JE Sargison, SM Guo, MLG Oldfield, GD Lock, AJ Rawlinson J. Turbomach. 124 (3), 453-460, 2002 | 290 | 2002 |
| Impulse response processing of transient heat transfer gauge signals MLG Oldfield | 271 | 2008 |
| Application of linear momentum actuator disc theory to open channel flow G Houlsby, S Draper, M Oldfield | 206 | 2008 |
| A converging slot-hole film-cooling geometry—part 2: transonic nozzle guide vane heat transfer and loss JE Sargison, SM Guo, MLG Oldfield, GD Lock, AJ Rawlinson J. Turbomach. 124 (3), 461-471, 2002 | 180 | 2002 |
| Simulation of the effects of shock wave passing on a turbine rotor blade DJ Doorly, MLG Oldfield | 176 | 1985 |
| Unsteady conjugate heat transfer modeling L He, MLG Oldfield | 172 | 2011 |
| Transonic turbine blade tip aerothermal performance with different tip gaps—part I: tip heat transfer Q Zhang, DO O’Dowd, L He, MLG Oldfield, PM Ligrani | 129 | 2011 |
| Modelling tidal energy extraction in a depth-averaged coastal domain S Draper, GT Houlsby, MLG Oldfield, AGL Borthwick IET renewable power generation 4 (6), 545-554, 2010 | 125 | 2010 |
| An examination of the contributions to loss on a transonic turbine blade in cascade DJ Mee, NC Baines, MLG Oldfield, TE Dickens | 123 | 1992 |
| The theory of advanced multi-layer thin film heat transfer gauges JE Doorly, MLG Oldfield International journal of heat and mass transfer 30 (6), 1159-1168, 1987 | 114 | 1987 |
| Instantaneous exhaust temperature measurements using thermocouple compensation techniques K Kar, S Roberts, R Stone, M Oldfield, B French SAE transactions, 652-673, 2004 | 90 | 2004 |
| Aerodynamic performance of an annular cascade of film cooled nozzle guide vanes under engine representative conditions CRB Day, MLG Oldfield, GD Lock Experiments in fluids 29, 117-129, 2000 | 90 | 2000 |
| On-line computer for transient turbine cascade instrumentation MLG Oldfield, TV Jones, DL Schultz IEEE Transactions on Aerospace and Electronic Systems, 738-749, 1978 | 88 | 1978 |
| Design of wide-bandwidth analogue circuits for heat transfer instrumentation in transient tunnels MLG Oldfield, HJ Burd, NG Doe University of Oxford Department of Engineering Science, 1990 | 83 | 1990 |
| Coolant passages for gas turbine components GD Lock, MLG Oldfield US Patent 6,241,468, 2001 | 79 | 2001 |
| PIV maps of tip leakage and secondary flow fields on a low-speed turbine blade cascade with moving end wall P Palafox, MLG Oldfield, JE LaGraff, TV Jones | 77 | 2008 |
| The application of thin-film technology to measure turbine-vane heat transfer and effectiveness in a film-cooled, engine-simulated environment SM Guo, CC Lai, TV Jones, MLG Oldfield, GD Lock, AJ Rawlinson International Journal of Heat and Fluid Flow 19 (6), 594-600, 1998 | 73 | 1998 |
| Aerothermal performance of a winglet at engine representative Mach and Reynolds numbers DO O’Dowd, Q Zhang, L He, MLG Oldfield, PM Ligrani, BCY Cheong, ... | 71 | 2011 |
| A new transient cascade facility for the measurement of heat transfer rates DL Schultz, TV Jones, MLG Oldfield, LC Daniels AGARD High Temp. Probl. in Gas Turbine Eng. 27 p(SEE N 78-21118 12-07), 1978 | 71 | 1978 |
| Flow visualisation of the external flow from a converging slot-hole film-cooling geometry JE Sargison, MLG Oldfield, SM Guo, GD Lock, AJ Rawlinson Experiments in Fluids 38, 304-318, 2005 | 70 | 2005 |
