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Adrian Pudsey
Adrian Pudsey
Associate Professor, RMIT University
Verified email at rmit.edu.au
Title
Cited by
Cited by
Year
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
1202010
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
642015
Hypersonic viscous drag reduction via multiporthole injector arrays
AS Pudsey, RR Boyce, V Wheatley
Journal of Propulsion and Power 29 (5), 1087-1096, 2013
542013
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
402013
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
332020
Cavity enhanced jet interactions in a scramjet combustor
T Roos, A Pudsey, M Bricalli, H Ogawa
Acta Astronautica 157, 162-179, 2019
262019
Supersonic boundary-layer combustion via multiporthole injector arrays
AS Pudsey, V Wheatley, RR Boyce
AIAA Journal 53 (10), 2890-2906, 2015
222015
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
132018
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
122021
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
122020
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
122019
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
102011
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
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
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
42020
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
32022
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
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
22022
Numerical investigation of upstream cavity enhanced combustion in a scramjet combustor
T Roos, AS Pudsey, M Bricalli, H Ogawa
23rd AIAA International Space Planes and Hypersonic Systems and Technologies …, 2020
22020
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
22018
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