ORCID as entered in ROS
https://orcid.org/0000-0003-0718-3324
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Conference Papers
, 2006, 'Numerical study of shock wave interactions around a transonic land speed record car', in Technical Committee (ed.), Shockwave Interaction, Rome, Italy, pp. 1 - 6, presented at
, 2006, 'The use of thermochromic liquid crystals to investigate flow field interaction with the ground around a supersonic land speed record vehicle', in 13th International Heat Transfer Conference, Sydney, presented at
, 2005, 'CFD analysis of an ethylene-fueled intake-injection shock-induced-combustion scramjet configuration', in A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference, pp. 329 - 345
, 2005, 'CFD analysis of nosecone geometries and a generic 2D scramjet', in A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference, pp. 1283 - 1308
, 2005, 'Flow studies on a hydrogen-fueled cavity flame-holder scramjet', in A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference, pp. 1478 - 1485
, 2005, 'Aerodynamics of land speed record vehicles', in Maruyama S (ed.), International COE of Flow Dynamics, Sendai, Japan, pp. 1 - 16, presented at
, 2005, 'Flow field studies of Axisymmetric and Rectangular Supersonic Under-Expanded Jets using a Gun Tunnel', in International Conference on Jets, Wakes and Separated Flows, Toba-shi, Mie, Japan, presented at
, 2005, 'Measurement of Gas Temperature Distributions in Flows using Radiating High-Porosity Meshes', in 5th Pacific Symposium on Flow Visualisation and Image Processing (PSFVIP-5-101), DayDream Island, Qld, presented at
, 2005, 'CFD Analysis of an ethylene-fueled intake-injection shock-induced-combustion scramjet configuration', in AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies, Capua, Italy, pp. 1 - 17, presented at
, 2005, 'CFD Analysis of the HyCAUSE Nosecone', in AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies, Capua, Italy, pp. 1 - 7, presented at
, 2005, 'Flow studies on a Hydrogen-fueled cavity Flame-Holder Scramjet', in AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies, Capua, Italy, pp. 1 - 16, presented at
, 2005, 'Heating Analysis of a Generic Scramjet', in AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies, Capua, Italy, pp. 1 - 12, presented at
, 2005, 'OH PLIF Imaging of Supersonic Combustion using Cavity Injection', in AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies, Capua, Italy, pp. 1 - 12, presented at
, 2005, 'OH PLIF imaging of supersonic combustion using cavity injection', in A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference, pp. 1466 - 1477, http://dx.doi.org/10.2514/6.2005-3357
, 2003, 'A novel liquid crystal image processing technique using multiple gas temperature steps to determine heat transfer coefficient distribution and adiabatic wall temperature', in American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI, pp. 123 - 131, http://dx.doi.org/10.1115/GT2003-38198
, 2003, 'Detailed investigation of heat flux measurements made in a standard propane-air fire-certification burner compared to levels derived from a low-temperature analogue burner', in American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI, pp. 169 - 177, http://dx.doi.org/10.1115/GT2003-38196
, 2003, 'Hydrocarbon and hydrogen-fuelled scramjet cavity flameholder performance at high flight mach numbers', in 12th AIAA International Space Planes and Hypersonic Systems and Technologies
, 2001, 'Compact low-temperature analogue of aero engine firecertification burner', in Proceedings of the ASME Turbo Expo, http://dx.doi.org/10.1115/2001-GT-0364
, 1999, 'Pilot study to investigate novel experimental and theoretical fire-event modelling techniques', in 37th Aerospace Sciences Meeting and Exhibit
, 1999, 'Pilot study to investigate novel experimental and theoretical fire-event modelling techniques', in 37th Aerospace Sciences Meeting and Exhibit
, 1999, 'Preliminary experimental investigation of acoustic liner heat passing capacity', in 5th AIAA/CEAS Aeroacoustics Conference and Exhibit
, 1999, 'Preliminary experimental investigation of acoustic liner heat passing capacity', in 5th AIAA/CEAS Aeroacoustics Conference and Exhibit
, 1998, 'Local coefficients of heat transfer on optimised finned cylinders', in 36th AIAA Aerospace Sciences Meeting and Exhibit, American Institute of Aeronautics and Astronautics, presented at
, 1997, 'Heat transfer coefficient distributions for the convective cooling of non-cylindrical geometries in crossflow using extended surfaces', in American Society of Mechanical Engineers (Paper)
, 1997, 'Local heat transfer coefficients on flat continuous, flat interrupted and corrugated external cooling fins', in American Society of Mechanical Engineers (Paper)
, 1997, 'Extended surface convective cooling studies of engine components using the transient liquid crystal technique', in Proceedings of the 1997 2nd European Conference on Turbomachinery - Fluid Dynamics and Thermodynamics, Antwerpen, Belgium, 5-7 March 1997, pp. 463 - 474
, 1997, 'Heat transfer coefficient distributions for the convective cooling of non-cylindrical geometries in crossflow using extended surfaces', in Proceedings of the ASME Turbo Expo, http://dx.doi.org/10.1115/97-GT-379
, 1997, 'Local heat transfer coefficients on flat continuous, flat interrupted and corrugated external cooling fins', in Proceedings of the ASME Turbo Expo, http://dx.doi.org/10.1115/97-GT-380
, 1994, 'Measurement of heating rates for earth entry at 13 kms-1', in AIAA 25th Plasmadynamics and Lasers Conference, 1994
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https://orcid.org/0000-0003-0718-3324