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Adrian Pudsey
Adrian Pudsey
Associate Professor, RMIT University
E-mail confirmado em rmit.edu.au
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Ano
Numerical investigation of transverse jets through multiport injector arrays in a supersonic crossflow
AS Pudsey, RR Boyce
Journal of Propulsion and Power 26 (6), 1225-1236, 2010
1462010
Behavior of multiple-jet interactions in a hypersonic boundary layer
AS Pudsey, V Wheatley, RR Boyce
Journal of Propulsion and Power 31 (1), 144-155, 2015
732015
Hypersonic viscous drag reduction via multiporthole injector arrays
AS Pudsey, RR Boyce, V Wheatley
Journal of Propulsion and Power 29 (5), 1087-1096, 2013
622013
Numerical investigation of upstream cavity enhanced fuel mixing in scramjet combustors
T Roos, A Pudsey, M Bricalli, H Ogawa
Acta Astronautica 169, 50-65, 2020
432020
Influence of common modeling choices for high-speed transverse jet-interaction simulations
AS Pudsey, RR Boyce, V Wheatley
Journal of Propulsion and Power 29 (5), 1076-1086, 2013
432013
Cavity enhanced jet interactions in a scramjet combustor
T Roos, A Pudsey, M Bricalli, H Ogawa
Acta Astronautica 157, 162-179, 2019
312019
Supersonic boundary-layer combustion via multiporthole injector arrays
AS Pudsey, V Wheatley, RR Boyce
AIAA Journal 53 (10), 2890-2906, 2015
282015
Numerical investigation of combustion characteristics of upstream crescent cavities in a scramjet combustor
T Roos, A Pudsey, H Ogawa
Acta Astronautica 187, 43-60, 2021
152021
Numerical investigation of fuel mixing with upstream crescent cavities in a scramjet combustor
T Roos, A Pudsey, M Bricalli, H Ogawa
Acta Astronautica 177, 611-626, 2020
142020
Scramjet performance with nonuniform flow and swept nozzles
MG Bricalli, L Brown, RR Boyce, R Gollan, T Vanyai, AS Pudsey
AIAA Journal 56 (10), 3988-4003, 2018
142018
Mixing characteristics of cracked gaseous hydrocarbon fuels in a scramjet combustor
M Ravindran, M Bricalli, A Pudsey, H Ogawa
Acta Astronautica 162, 168-184, 2019
132019
Full flow-path optimization of axisymmetric scramjet engines
H Ogawa, Y Alazet, A Pudsey, R Boyce, A Isaacs, T Ray
17th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2011
122011
SCRAMSPACE: Radical-Farming Scramjet for access to space
S Tirtey, R Boyce, M Brown, B Capra, M Creagh, A Dedman, I Dimitrijevic, ...
Hypersonic Flight Testing, 1-31, 2014
72014
Heat flux measurements of a methane-oxygen rotating detonation rocket engine
R Aliakbari, Q Michalski, N Mason-Smith, A Pudsey, M Wenzel, N Paull
International Workshop on Detonation Propulsion, 2022
62022
Analysis of a multi-porthole injector array in a supersonic crossflow
MG Bricalli, M Pfeiffer, AS Pudsey, K Basore
Journal of Propulsion and Power 36 (4), 560-574, 2020
62020
Structure of rotating detonation in mixtures of natural gas and oxygen
Q Michalski, R Aliakbari, N Mason-Smith, N Paull, M Wenzel, A Pudsey
Combustion and Flame 260, 113253, 2024
52024
Mixing enhancement in a hydrocarbon-fuelled scramjet engine through repeated laser sparks
F Rogg, M Bricalli, S O'Byrne, AS Pudsey, P Marzocca
23rd AIAA International Space Planes and Hypersonic Systems and Technologies …, 2020
52020
Impact of life cycle assessment considerations on launch vehicle design
T Bellier, A Urbano, J Morlier, C Bil, A Pudsey
73rd International Astronautical Congress (IAC) 2022–Paris, France, 2022
42022
Numerical simulations of radiative heat effects in a plasma wind-tunnel flow under Mars entry conditions
J García-Garrido, AS Pudsey, C Mundt
Acta Astronautica 151, 334-341, 2018
42018
Laser-induced fluorescence investigations for temperature measurements in a carbon dioxide flow
M Kirschner, AS Pudsey, F Koroll, T Sander, C Mundt
Journal of Thermophysics and Heat Transfer 32 (1), 216-225, 2018
32018
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