Dynamic behaviour of auxetic gradient composite hexagonal honeycombs L Boldrin, S Hummel, F Scarpa, D Di Maio, C Lira, M Ruzzene, ... Composite Structures 149, 114-124, 2016 | 179 | 2016 |
Fretting fatigue in dovetail blade roots: Experiment and analysis R Rajasekaran, D Nowell Tribology international 39 (10), 1277-1285, 2006 | 171 | 2006 |
A gradient cellular core for aeroengine fan blades based on auxetic configurations C Lira, F Scarpa, R Rajasekaran Journal of Intelligent Material Systems and Structures 22 (9), 907-917, 2011 | 162 | 2011 |
Efficient computational techniques for mistuning analysis of bladed discs: a review J Yuan, F Scarpa, G Allegri, B Titurus, S Patsias, R Rajasekaran Mechanical Systems and Signal Processing 87, 71-90, 2017 | 68 | 2017 |
Effective topologies for vibration damping inserts in honeycomb structures MA Boucher, CW Smith, F Scarpa, R Rajasekaran, KE Evans Composite Structures 106, 1-14, 2013 | 54 | 2013 |
Vibration damping structures F Scarpa, CW Smith, W Miller, K Evans, R Rajasekaran US Patent 9,382,962, 2016 | 46 | 2016 |
Dynamics of dry friction damping in gas turbines: literature survey A Rizvi, CW Smith, R Rajasekaran, KE Evans Journal of Vibration and Control 22 (1), 296-305, 2016 | 43 | 2016 |
On the finite element analysis of contacting bodies using submodelling R Rajasekaran, D Nowell The Journal of strain analysis for engineering design 40 (2), 95-106, 2005 | 35 | 2005 |
Vibration damping R Rajasekaran, M Boucher, CW Smith, F Scarpa, KE Evans US Patent 9,494,206, 2016 | 29 | 2016 |
Probabilistic dynamics of mistuned bladed disc systems using subset simulation J Yuan, G Allegri, F Scarpa, R Rajasekaran, S Patsias Journal of Sound and Vibration 350, 185-198, 2015 | 29 | 2015 |
Novel parametric reduced order model for aeroengine blade dynamics J Yuan, G Allegri, F Scarpa, R Rajasekaran, S Patsias Mechanical Systems and Signal Processing 62, 235-253, 2015 | 24 | 2015 |
Thermal conductivities of iso-volume centre-symmetric honeycombs L Boldrin, F Scarpa, R Rajasekaran Composite Structures 113, 498-506, 2014 | 19 | 2014 |
A novel hybrid Neumann expansion method for stochastic analysis of mistuned bladed discs J Yuan, G Allegri, F Scarpa, S Patsias, R Rajasekaran Mechanical Systems and Signal Processing 72, 241-253, 2016 | 18 | 2016 |
Novel frame model for mistuning analysis of bladed disk systems J Yuan, F Scarpa, B Titurus, G Allegri, S Patsias, R Rajasekaran Journal of Vibration and Acoustics 139 (3), 031016, 2017 | 15 | 2017 |
A correlation of the process zone properties in complete, incomplete and almost complete fretting contacts D Dini, C Churchman, R Rajasekaran, DA Hills International journal of mechanical sciences 46 (3), 491-508, 2004 | 10 | 2004 |
Numerical Assessment of Using Sherman-Morrison, Neumann Expansion Techniques for Stochastic Analysis of Mistuned Bladed Disc System J Yuan, F Scarpa, G Allegri, S Patsias, R Rajasekaran Turbo Expo: Power for Land, Sea, and Air 56772, V07BT32A021, 2015 | 9 | 2015 |
Vibration damping structures R Rajasekaran, FL Scarpa, KE Evans, CW Smith, W Miller EP Patent App. 2011/051,790, 2011 | 5 | 2011 |
Analysis of dovetails for fretting fatigue R Rajasekaran University of Oxford, 2005 | 2 | 2005 |
Novel parametric reduced order model for aeroengine blade dynamics J Yuan, G Allegri, F Scarpa, R Rajasekaran Dynamics of Coupled Structures, Volume 1: Proceedings of the 32nd IMAC, A …, 2014 | 1 | 2014 |
Characteristics of the state of stress at the edge of a titled punch R Rajasekaran, DA Hills The Journal of Strain Analysis for Engineering Design 41 (1), 1-7, 2006 | | 2006 |