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Shannon Ryan
Shannon Ryan
Applied Artificial Intelligence Institute (A2I2), Deakin University
Verified email at deakin.edu.au
Title
Cited by
Cited by
Year
Handbook for Designing MMOD Protection
EL Christiansen, J Arnold, B Corsaro, A Davis, F Giovane, J Hyde, D Lear, ...
NASA Johnson Space Center, NASA/TM-2009-214785, 2009
1382009
The effect of target thickness on the ballistic performance of ultra high molecular weight polyethylene composite
LH Nguyen, S Ryan, SJ Cimpoeru, AP Mouritz, AC Orifici
International Journal of Impact Engineering 75, 174-183, 2015
1112015
Hypervelocity impact on CFRP: testing, material modelling, and numerical simulation
M Wicklein, S Ryan, DM White, RA Clegg
International Journal of Impact Engineering 35 (12), 1861-1869, 2008
1092008
A ballistic limit equation for hypervelocity impacts on composite honeycomb sandwich panel satellite structures
S Ryan, F Schaefer, R Destefanis, M Lambert
Advances in Space Research 41 (7), 1152-1166, 2008
952008
A methodology for hydrocode analysis of ultra-high molecular weight polyethylene composite under ballistic impact
LH Nguyen, TR Lässig, S Ryan, W Riedel, AP Mouritz, AC Orifici
Composites Part A: Applied Science and Manufacturing 84, 224-235, 2016
722016
Hypervelocity impact testing of advanced materials and structures for micrometeoroid and orbital debris shielding
S Ryan, EL Christiansen
Acta Astronautica 83, 216-231, 2013
642013
Theoretical prediction of dynamic composite material properties for hypervelocity impact simulations
S Ryan, M Wicklein, A Mouritz, W Riedel, F Schäfer, K Thoma
International Journal of Impact Engineering 36 (7), 899-912, 2009
582009
Honeycomb vs. foam: Evaluating potential upgrades to ISS module shielding
S Ryan, T Hedman, EL Christiansen
Acta Astronautica 67 (7-8), 818-825, 2010
562010
Numerical simulation of hypervelocity impact on CFRP/Al HC SP spacecraft structures causing penetration and fragment ejection
S Ryan, F Schaefer, W Riedel
International journal of impact engineering 33 (1-12), 703-712, 2006
542006
Micrometeoroid and orbital debris (MMOD) shield ballistic limit analysis program
S Ryan, EL Christiansen
Johnson Space Center, 2010
502010
The ballistic performance of an ultra-high hardness armour steel: An experimental investigation
S Ryan, H Li, M Edgerton, D Gallardy, SJ Cimpoeru
International journal of impact engineering 94, 60-73, 2016
472016
Ballistic limit equation for equipment placed behind satellite structure walls
FK Schäfer, S Ryan, M Lambert, R Putzar
International Journal of Impact Engineering 35 (12), 1784-1791, 2008
432008
Numerical modelling of ultra-high molecular weight polyethylene composite under impact loading
LH Nguyen, TR Lässig, S Ryan, W Riedel, AP Mouritz, AC Orifici
Procedia Engineering 103, 436-443, 2015
332015
A ballistic limit analysis programme for shielding against micrometeoroids and orbital debris
S Ryan, EL Christiansen
Acta Astronautica 69 (5-6), 245-257, 2011
312011
Whipple shield performance in the shatter regime
S Ryan, M Bjorkman, EL Christiansen
International Journal of Impact Engineering 38 (6), 504-510, 2011
272011
Characterizing the transient response of CFRP/Al HC spacecraft structures induced by space debris impact at hypervelocity
S Ryan, F Schäfer, M Guyot, S Hiermaier, M Lambert
International Journal of Impact Engineering 35 (12), 1756-1763, 2008
272008
Hypervelocity impact testing of CFRP/Al honeycomb satellite structures
F Schäfer, R Destefanis, S Ryan, W Riedel, M Lambert
4th European conference on space debris 587, 407, 2005
272005
The efficiency of ultra-high molecular weight polyethylene composite against fragment impact
LH Nguyen, S Ryan, SJ Cimpoeru, AP Mouritz, AC Orifici
Experimental mechanics 56 (4), 595-605, 2016
252016
Physical mechanisms for near-field blast mitigation with fluid containers: Effect of container geometry
H Bornstein, S Ryan, A Mouritz
International journal of impact engineering 96, 61-77, 2016
232016
Machine learning methods for predicting the outcome of hypervelocity impact events
S Ryan, S Thaler, S Kandanaarachchi
Expert Systems with Applications 45, 23-39, 2016
222016
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