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Ramesh Rajasekaran
Ramesh Rajasekaran
TerraPower, Rolls-Royce plc, University of Oxford
Verified email at TerraPower.com - Homepage
Title
Cited by
Cited by
Year
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
1772016
Fretting fatigue in dovetail blade roots: Experiment and analysis
R Rajasekaran, D Nowell
Tribology international 39 (10), 1277-1285, 2006
1712006
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
1612011
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
662017
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
532013
Vibration damping structures
F Scarpa, CW Smith, W Miller, K Evans, R Rajasekaran
US Patent 9,382,962, 2016
452016
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
422016
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
342005
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
292015
Vibration damping
R Rajasekaran, M Boucher, CW Smith, F Scarpa, KE Evans
US Patent 9,494,206, 2016
282016
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
242015
Thermal conductivities of iso-volume centre-symmetric honeycombs
L Boldrin, F Scarpa, R Rajasekaran
Composite Structures 113, 498-506, 2014
192014
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
182016
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
152017
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
102004
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
92015
Vibration damping structures
R Rajasekaran, FL Scarpa, KE Evans, CW Smith, W Miller
EP Patent App. 2011/051,790, 2011
52011
Analysis of dovetails for fretting fatigue
R Rajasekaran
University of Oxford, 2005
22005
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
12014
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
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