Article

Goodhand, MN and Miller, RJ (2012) The Impact of Real Geometries on Three-Dimensional Separations in Compressors. J TURBOMACH, 134. -. ISSN 0889-504X

Goodhand, MN and Miller, RJ (2011) Compressor Leading Edge Spikes: A New Performance Criterion. J TURBOMACH, 133. -. ISSN 0889-504X

Massini, M and Miller, RJ and Hodson, HP (2011) A New Intermittent Aspirated Probe for the Measurement of Stagnation Quantities in High Temperature Gases. J TURBOMACH, 133. -. ISSN 0889-504X

Atkins, NR and Miller, RJ and Ainsworth, RW (2011) The development of aerodynamic performance measurements in a transient test facility. Proceedings of the ASME Turbo Expo 2004, 5 B. pp. 1325-1338.

Ward, CM and Duffin, M and Miller, RJ and Heffer, JJH (2010) Unsteady ejectors: The effect of driver jet mark-space ratio. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.

Ong, J and Miller, RJ and Denton, JD (2010) The prediction of hot streak migration in a high-pressure turbine. P I MECH ENG A-J POW, 224. pp. 119-128. ISSN 0957-6509

Ong, J and Miller, RJ and Denton, JD (2010) The prediction of hot streak migration in a high-pressure turbine. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 224. pp. 119-128. ISSN 0957-6509

Heffer, JJH and Miller, RJ (2010) A transonic vane for use downstream of a pressure gain combustor. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.

Wheeler, APS and Sofia, A and Miller, RJ (2009) The Effect of Leading-Edge Geometry on Wake Interactions in Compressors. J TURBOMACH, 131. -. ISSN 0889-504X

Heffer, JJH and Miller, RJ (2009) Performance of choked unsteady ejector-nozzles for use in pressure-gain combustors. 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.

Wheeler, APS and Miller, RJ (2008) Compressor wake/leading-edge interactions at off design incidences. Proceedings of the ASME Turbo Expo, 6. pp. 1795-1806.

Mason, SA and Miller, RJ and Taylor, MD (2008) Fluid mechanics of pulse pressure-gain combustors. 46th AIAA Aerospace Sciences Meeting and Exhibit.

Ong, J and Miller, RJ (2008) Hot streak and vane coolant migration in a downstream rotor. Proceedings of the ASME Turbo Expo, 6.

Heffer, JJH and Miller, RJ and Freeman, C (2008) The time-resolved flow within an unsteady ejector. 46th AIAA Aerospace Sciences Meeting and Exhibit.

Atkins, NR and Miller, RJ and Ainsworth, RW (2007) The development of aerodynamic performance measurements in a transient test facility. Transactions of the ASME, Journal of Turbomachinery. ISSN 0889-504X

Miller, RJ and Moss, RW and Ainsworth, RW and Harvey, NW (2007) The effect of an upstream turbine on a low-aspect ratio vane. Transactions of the ASME, Journal of Turbomachinery. ISSN 0889-504X

Wheeler, AP and Sofia, A and Miller, RJ (2007) The effect of leading-edge geometry on wake interactions in compressors. Transactions of the ASME, Journal of Turbomachinery. ISSN 0889-504X

Wheeler, AP and Miller, RJ and Hodson, HP (2007) The effect of wake induced coherent structures on compressor boundary layers. Transactions of the ASME, Journal of Turbomachinery, 129. ISSN 0889-504X

Thorpe, SJ and Miller, RJ and Yoshino, S and Ainsworth, RW and Harvey, NW (2007) The effect of work processes on the casing heat transfer of a transonic turbine. ASME Transactions, Journal of Turbomachinery, 129. pp. 84-91. ISSN 0889-504X

Mason, SA and Miller, RJ (2006) The performance of ejectors driven by sinusoidally unsteady jets. Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting, 16. pp. 12245-12255.

Payne, SJ and Ainsworth, RW and Miller, RJ and Moss, RW and Harvey, NW (2005) Unsteady loss in a high pressure turbine stage: interaction effects. International Journal of Heat and Fluid Flow, 26. pp. 695-708. ISSN 0142-727X

Thorpe, SJ and Miller, RJ and Yoshino, S and Ainsworth, RW and Harvey, NW (2005) The effect of work processes on the casing heat transfer of a transonic turbine. Proceedings of the ASME Turbo Expo, 3 PART. pp. 443-451.

Miller, RJ and Ainsworth, RW and Moss, RW and Harvey, NW (2004) The effect of an upstream turbine on a low-aspect ratio vane. Proceedings of the ASME Turbo Expo 2004, 5 B. pp. 1417-1428.

Miller, RJ and Moss, RW and Ainsworth, RW and Horwood, CK (2003) Time-resolved vane-rotor interaction in a high-pressure turbine stage. ASME Transactions, Journal of Turbomachinery, 125. pp. 1-13. ISSN 0889-504X

Payne, SJ and Ainsworth, RW and Miller, RJ and Moss, RW and Harvey, NW (2003) Unsteady loss in a high pressure turbine stage. International Journal of Heat and Fluid Flow, 24. pp. 698-708. ISSN 0142-727X

Miller, RJ and Moss, RW and Ainsworth, RW and Harvey, NW (2003) Wake, shock and potential field interactions in a 1.5 stage turbine - Part I: Vane-rotor and rotor-vane interaction. ASME Transactions, Journal of Turbomachinery, 125. pp. 33-39. ISSN 0889-504X

Miller, RJ and Moss, RW and Ainsworth, RW and Harvey, NW (2003) Wake, shock and potential field interactions in a 1.5 stage turbine - Part II: Vane-vane interactions and discussion of results. ASME Transactions, Journal of Turbomachinery, 125. pp. 40-47. ISSN 0889-504X

Miller, RJ and Moss, RW and Ainsworth, RW and Harvey, NW (2003) The development of turbine exit flow in a swan-necked inter-stage diffuser. American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI, 6 B. pp. 863-875.

Miller, RJ and Moss, RW and Ainsworth, RW and Harvey, NW (2002) Wake, shock and potential field interactions in a 1.5 stage turbine: Part I: Vane-rotor and rotor-vane interaction. American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI, 5 B. pp. 715-723.

Miller, RJ and Moss, RW and Ainsworth, RW and Harvey, NW (2002) Wake, shock and potential field interactions in a 1.5 stage turbine: Part II: Vane-vane interaction and discussion of results. American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI, 5 B. pp. 725-734.

Miller, RJ and Moss, RW and Ainsworth, RW and Harvey, NW (2001) Time-resolved vane-rotor-vane interaction in a transonic one-and-a-half stage turbine. Proceedings of Institution of Mechanical Engineers, PT A: Journal of Power and Energy, 215. pp. 675-685. ISSN 0957-6509

Ainsworth, RW and Miller, RJ and Moss, RW and Thorpe, SJ (2000) Unsteady pressure measurement. Measurement Science and Technology, 11. pp. 1055-1076. ISSN 0957-0233

Collings, N and Massini, M and Hodson, HP and Miller, RJ A new Intermittent Aspirated Probe for the Measurement of Stagnation Quantities in High Temperature Gases. (Unpublished)

Conference or Workshop Item

Naylor, EMJ and Duenas, CO and Miller, RJ and Hodson, HP (2010) Optimization of Nonaxisymmetric Endwalls in Compressor S-Shaped Ducts. In: UNSPECIFIED -..

Karakasis, MK and Naylor, EMJ and Miller, RJ and Hodson, HP (2010) THE EFFECT OF AN UPSTREAM COMPRESSOR ON A NON-AXISYMMETRIC S-DUCT. In: UNSPECIFIED pp. 477-486..

Goodhand, MN and Miller, RJ (2010) THE IMPACT OF REAL GEOMETRIES ON THREE-DIMENSIONAL SEPARATIONS IN COMPRESSORS. In: UNSPECIFIED pp. 129-138..

Massini, M and Miller, RJ and Hodson, HP and Collings, N (2010) A NOVEL TECHNIQUE FOR MEASURING STAGNATION QUANTITIES AND GAS COMPOSITION IN HIGH TEMPERATURE FLOWS. In: UNSPECIFIED pp. 223-233..

Goodhand, MN and Miller, RJ (2009) COMPRESSOR LEADING EDGE SPIKES: A NEW PERFORMANCE CRITERION. In: UNSPECIFIED pp. 1553-1562..

Naylor, EMJ and Ortiz Duenas, C and Miller, RJ and Hodson, H (2008) Optimisation of non-axisymmetric endwalls in compressor S-shaped ducts. In: ASME Turbo Expo 2008, 9-5-2008 to 13-5-2008, Berlin, Germany.

Massini, M and Miller, RJ and Hodson, H (2008) A new intermittent aspirated probe for the measurement of stagnation quantities in high temperature gases. In: ASME Turbo Expo 2008, 9-5-2008 to 13-5-2008, Berlin, Germany.

Ong, J and Miller, RJ (2008) HOT STREAK AND VANE COOLANT MIGRATION IN A DOWNSTREAM ROTOR. In: UNSPECIFIED pp. 1749-1760..

Offord, T and Miller, RJ and Dawson, JR and Heffer, JJH and Mason, S and Taylor, M (2008) Improving the performance of a valveless pulse combustor using unsteady fuel injection. In: UNSPECIFIED.

Massini, M and Miller, RJ and Hodson, HP (2008) A NEW INTERMITTENT ASPIRATED PROBE FOR THE MEASUREMENT OF STAGNATION QUANTITIES IN HIGH TEMPERATURE GASES. In: UNSPECIFIED pp. 145-152..

Naylor, EMJ and Duenas, CO and Miller, RJ and Hodson, HP (2008) OPTIMISATION OF NON-AXISYMMETRIC ENDWALLS IN COMPRESSOR S-SHAPED DUCTS. In: UNSPECIFIED pp. 305-316..

Ortiz Duenas, C and Miller, RJ and Hodson, HP and Longley, JP (2007) Effect of length on compressor inter-stage duct performance. In: ASME Turbo Exposition 2007, 14-5-2007 to 17-5-2007, Montreal, Canada.

Wheeler, AP and Sofia, A and Miller, RJ (2007) Effect of length on compressor inter-stage duct performance. In: ASME Turbo Expo - Power for Land, Sea and Air, 14-5-2007 to 17-5-2007, Montreal, Canada.

Wheeler, APS and Miller, RJ and Hodson, HP (2007) The effect of wake induced structures on compressor boundary-layers. In: UNSPECIFIED pp. 705-712..

Thorpe, SJ and Miller, RJ and Yoshino, S and Ainsworth, RW and Harvey, NW (2007) The effect of work processes on the casing heat transfer of a transonic turbine. In: UNSPECIFIED pp. 84-91..

Duenas, CO and Miller, RJ and Hodson, HP and Longley, JP (2007) Effect of length on compressor inter-stage duct performance. In: UNSPECIFIED pp. 319-329..

Wheeler, APS and Sofia, A and Miller, RJ (2007) The effect of leading-edge geometry on wake interactions in compressors. In: UNSPECIFIED pp. 1769-1779..

Wheeler, AP and Miller, RJ and Hodson, HP (2006) The effect of wake induced coherent structures on compressor boundary layers. In: ASME Turbo Expo - Power for Land Sea and Air, 8-5-2006 to 11-5-2006, Barcelona, Spain.

Wheeler, APS and Miller, RJ and Hodson, HP (2006) The effect of wake induced structures on compressor boundary layers. In: ASME Turbo Expo, 8-5-2006 to 11-5-2006, Barcelona, Spain.

Ong, J and Miller, RJ and Uchida, S (2006) The effect of coolant injection on the endwall flow of a high pressure turbine. In: ASME Turbo Exposition, -5-2006 to --, Barcelona, Spain.

Mason, SA and Miller, RJ (2006) An investigation into the performance of ejectors driven by sinusoidally unsteady jets. In: 44th AIAA Aerospace Sciences Meeting and Exhibit, 9-1-2006 to 12-1-2006, Reno, Nevada.

Ong, JHP and Miller, RJ and Uchida, S (2006) The effect of coolant injection on the endwall flow of a high pressure turbine. In: UNSPECIFIED pp. 915-924..

Wheeler, APS and Miller, RJ and Hodson, HP (2006) The effect of wake induced structures on compressor boundary-layers. In: UNSPECIFIED pp. 1875-1885..

Thorpe, SJ and Miller, RJ and Yoshino, S and Ainsworth, RW and Harvey, NW (2005) The effect of work processes on the casing heat transfer of a transonic turbine. In: ASME Turbo Expo - Power for Land, Sea and Air, 6-6-2005 to 9-6-2005, Reno, Nevada.

Appukuttan, A and Miller, RJ and Hodson, HP (2004) Probe measurement error in shear flows. In: The 17th Symposium on Measuring Techniques in Transonic and Supersonic Flow in Cascades and Turbomachines, 9-9-2004 to 10-9-2004, Stockholm, Sweden.

Atkins, NR and Miller, RJ and Ainsworth, RW (2004) The development of aerodynamic performance measurements in a transient test facility. In: ASME Turbo Expo - Power for Land, Sea and Air, 14-6-2004 to 17-6-2004, Vienna, Austria.

Miller, RJ and Moss, RW and Ainsworth, RW and Harvey, NW (2004) The effect of an upstream turbine on a low-aspect ratio vane. In: ASME Turbo Expo - Power for Land, Sea and Air, 14-6-2004 to 17-6-2004, Vienna, Austria.

Miller, RJ and Moss, RW and Ainsworth, RW and Harvey, NW (2003) The development of turbine exit flow in a swan-necked inter-stage diffuser. In: ASME Turbo Expo - Power for Land Sea and Air, 16-6-2003 to 19-6-2003, Atlanta, Georgia.

Yang, X and Miller, RJ and Hodson, HP (2002) A new probe for the measurement of high-temperature gases. In: XVIth Bi-Annual symposium on measuring techniques in transonic and supersonic flows in cascades and turbomachines, 23-9-2002 to 24-9-2002, Cambridge, UK.

Yang, X and Miller, RJ and Hodson, HP (2002) A new probe for the measurement of high-temperature gases. In: 16th Symposium on Measuring Techniques in Transonic and Supersonic Flow in Cascades and Turbomachines, 23-9-2002 to 24-9-2002, Cambridge, UK.

Miller, RJ and Moss, RW and Ainsworth, RW and Harvey, NW (2002) The effects of wake, shock and potential field interactions on the rotor of a 1.5 stage turbine: part 1 vane-rotor and rotor-vane interaction. In: ASME Turbo Expo - Power for Land Sea and Air, 3-6-2002 to 6-6-2002, Amsterdam, Netherlands.

Miller, RJ and Moss, RW and Ainsworth, RW and Harvey, NW (2002) The effects of wake, shock and potential field interactions on the rotor of a 1.5 stage turbine: part 2 vane-vane interaction and discussion of results. In: ASME Turbo Expo - Power for Land Sea and Air, 3-6-2002 to 6-6-2002, Amsterdam, Netherlands.

Miller, RJ and Moss, RW and Ainsworth, RW and Harvey, NW (2001) Time-resolved vane-rotor-vane interaction in a transonic one-and-a-half stage turbine. In: 4th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics (Euroturbo 4), 20-3-2001 to 23-3-2001, Florence, Italy pp. 937-949..

Miller, RJ and Moss, RW and Ainsworth, RW and Harvey, NW (2001) Time-resolved vane-rotor-vane interaction in a transonic one-and-a-half stage turbine. In: UNSPECIFIED pp. 675-685..

Moss, RW and Ainsworth, RW and Sheldrake, CD and Miller, RJ (1997) The unsteady pressure field over a turbine blade surface: visualisation and interpretation of experimental data. In: ASME Turbo Expo 1997: Power for Land, Sea and Air, 2-6-1997 to 5-6-1997, Orlando, Florida.

Miller, RJ and Ainsworth, RW (1996) An ultra-high speed traverse system for fast response aerodynamic measurements in transonic flow facilities. In: 13th Symposium on Measuring techniques for transonic and supersonic flow in cascades and turbomachines, 5-9-1996 to 6-9-1996, Zurich, Switzerland.