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Russell Boyce; RR Boyce; R Boyce
Russell Boyce; RR Boyce; R Boyce
Verified email at adfa.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
1352010
The HyShot scramjet flight experiment-flight data and CFD calculations compared
R Boyce, S Gerard, A Paull
12th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2003
992003
OH PLIF imaging of supersonic combustion using cavity injection
S O'Byrne, I Stotz, A Neely, R Boyce, N Mudford, F Houwing
AIAA/CIRA 13th International Space Planes and Hypersonics Systems and …, 2005
842005
Inlet starting of high-contraction axisymmetric scramjets
H Ogawa, AL Grainger, RR Boyce
Journal of Propulsion and Power 26 (6), 1247-1258, 2010
732010
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
662015
Physical insight into scramjet inlet behavior via multi-objective design optimization
H Ogawa, RR Boyce
AIAA journal 50 (8), 1773-1783, 2012
622012
SCRAMSPACE: scramjet-based access-to-space systems
R Boyce, S Tirtey, L Brown, M Creagh, H Ogawa
17th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2011
622011
Radical-farm ignition processes in two-dimensional supersonic combustion
JR McGuire, RR Boyce, NR Mudford
Journal of Propulsion and Power 24 (6), 1248-1257, 2008
622008
Hypersonic viscous drag reduction via multiporthole injector arrays
AS Pudsey, RR Boyce, V Wheatley
Journal of Propulsion and Power 29 (5), 1087-1096, 2013
572013
Comparison of supersonic combustion between impulse and vitiation-heated facilities
RR Boyce, A Paull, RJ Stalker, M Wendt, N Chinzei, H Miyajima
Journal of Propulsion and Power 16 (4), 709-717, 2000
532000
Validation study of numerical simulations by comparison to measurements in piston-driven shock-tunnels
C Mundt, R Boyce, P Jacobs, K Hannemann
Aerospace Science and Technology 11 (2-3), 100-109, 2007
502007
Scramjet performance for ideal combustion processes
T Vanyai, M Bricalli, S Brieschenk, RR Boyce
Aerospace Science and Technology 75, 215-226, 2018
492018
Nozzle design optimization for axisymmetric scramjets by using surrogate-assisted evolutionary algorithms
H Ogawa, RR Boyce
Journal of Propulsion and Power 28 (6), 1324-1338, 2012
462012
Simulations of mixing in an inlet-fueled axisymmetric scramjet
DM Peterson, RR Boyce, V Wheatley
AIAA journal 51 (12), 2823-2832, 2013
432013
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
Evolutionary algorithm shape optimization of a hypersonic flight experiment nose cone
NR Deepak, T Ray, RR Boyce
Journal of Spacecraft and Rockets 45 (3), 428-437, 2008
432008
Mass spectrometric measurements of driver gas arrival in the T4 free-piston shock-tunnel
RR Boyce, M Takahashi, RJ Stalker
Shock Waves 14, 371-378, 2005
412005
Numerical investigation of wall temperature and entropy layer effects on double wedge shock/boundary layer interactions
B Reinartz, J Ballmann, R Boyce
14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies …, 2006
332006
pdFOAM: A PIC-DSMC code for near-Earth plasma-body interactions
CJ Capon, M Brown, C White, T Scanlon, RR Boyce
Computers & Fluids 149, 160-171, 2017
322017
OH-PLIF visualisation of radical farming supersonic combustion flows
RR Boyce, NR Mudford, JR McGuire
Shock Waves 22, 9-21, 2012
292012
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