Adrian Pudsey
Adrian Pudsey
Lecturer, RMIT University
Verified email at rmit.edu.au - Homepage
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
792010
Numerical Analysis of Multi-Port Injection Arrays Into a Supersonic Crossflow
AS Pudsey, RR Boyce
15th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2008
79*2008
Behavior of Multiple-Jet Interactions in a Hypersonic Boundary Layer
A Pudsey, V Wheatley, R Boyce
Journal of Propulsion and Power 31 (1), 144-155, 2015
472015
Hypersonic viscous drag reduction via multiporthole injector arrays
AS Pudsey, RR Boyce, V Wheatley
Journal of Propulsion and Power 29 (5), 1087-1096, 2013
392013
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
342013
Supersonic boundary-layer combustion via multiporthole injector arrays
AS Pudsey, V Wheatley, RR Boyce
AIAA Journal 53 (10), 2890-2906, 2015
152015
Shock tunnel and numerical studies of a large inlet-fuelled inward turning axisymmetric scramjet
RR Boyce, JM Schramm, D Oberg, K Hannemann, L Brown
18th AIAA/3AF International Space Planes and Hypersonic Systems and …, 2012
122012
Cavity enhanced jet interactions in a scramjet combustor
T Roos, A Pudsey, M Bricalli, H Ogawa
Acta Astronautica 157, 162-179, 2019
92019
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
92011
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
82020
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
62014
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
52019
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
52018
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
12020
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
12018
Mixing characteristics of cracked gaseous hydrocarbon fuels in scramjets
MR Ravindran, M Bricalli, A Pudsey, H Ogawa
22nd AIAA International Space Planes and Hypersonics Systems and …, 2018
12018
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
12018
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
2020
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
2020
Numerical simulation of the effects of a single laser spark on the dynamics of a hydrocarbon fuelled scramjet combustor
F Rogg, M Bricalli, S O'Byrne, A Pudsey, P Marzocca
APISAT 2019: Asia Pacific International Symposium on Aerospace Technology, 1747, 2019
2019
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Articles 1–20