| A review of multifunctional structure technology for aerospace applications KK Sairajan, GS Aglietti, KM Mani Acta astronautica 120, 30-42, 2016 | 143 | 2016 |
| Vibration suppression of printed circuit boards using an external particle damper P Veeramuthuvel, KK Sairajan, K Shankar Journal of Sound and Vibration 366, 98-116, 2016 | 46 | 2016 |
| Robustness of system equivalent reduction expansion process on spacecraft structure model validation KK Sairajan, GS Aglietti AIAA journal 50 (11), 2376-2388, 2012 | 35 | 2012 |
| Application of particle damper on electronic packages for spacecraft P Veeramuthuvel, K Shankar, KK Sairajan Acta Astronautica 127, 260-270, 2016 | 33 | 2016 |
| Design of low mass dimensionally stable composite base structure for a spacecraft KK Sairajan, PS Nair Composites Part B: Engineering 42 (2), 280-288, 2011 | 24 | 2011 |
| Experimental investigation of particle damper-based vibration suppression in printed circuit board for spacecraft applications P Veeramuthuvel, K Shankar, KK Sairajan Proceedings of the Institution of Mechanical Engineers, Part g: Journal of …, 2016 | 17 | 2016 |
| Application of RBF neural network in prediction of particle damping parameters from experimental data P Veeramuthuvel, K Shankar, KK Sairajan Journal of Vibration and Control 23 (6), 909-929, 2017 | 14 | 2017 |
| Study of correlation criteria for base excitation of spacecraft structures KK Sairajan, GS Aglietti Journal of Spacecraft and Rockets 51 (1), 106-116, 2014 | 11 | 2014 |
| Correlation of finite element models of multi-physics systems KK Sairajan, GS Aglietti, SJI Walker Journal of Sound and Vibration 333 (17), 4051-4070, 2014 | 10 | 2014 |
| Prediction of particle damping parameters using RBF neural network P Veeramuthuvel, K Shankar, KK Sairajan, R Machavaram Procedia Materials Science 5, 335-344, 2014 | 10 | 2014 |
| Optimum design of a composite base structure of a spacecraft KK Sairajan, PS Shamnad, K Thomas, N Joseph Altair CAE Users Conference, 11-13, 2005 | 4 | 2005 |
| Validity of model correlation methods in FEM validation for forced vibration analysis KK Sairajan, GS Aglietti 12th European Conference on Spacecraft Structures, Materials and …, 2012 | 3 | 2012 |
| Use of Base Force Assurance Criterion for Spacecraft Structure Model Correlation KK Sairajan, MNM Patnaik, SS Narayan, S Deshpande, D Premkumar AIAA: American Institute of Aeronautics and Astronautics, 2015 | 2 | 2015 |
| Base force and moment based finite element model correlation method KK Sairajan, SS Deshpande, MNM Patnaik, D Poomani Advances in Space Research 68 (10), 4056-4068, 2021 | 1 | 2021 |
| Correlation aspects of spacecraft and multi-physics finite element models KK Sairajan University of Southampton, 2013 | 1 | 2013 |
| Standard FEM validation checks and quality of response prediction KK Sairajan, GS Aglietti Proceedings of the International Astronautical Congress, IAC 8, 6216-6222, 2012 | 1 | 2012 |
| Correlation of finite element model of a Piezoelectric system KK Sairajan, GS Aglietti, SJI Walker | | 2013 |
| A SUBSTRUCTURAL ANALYTICAL METHOD FOR MICRO-VIBRATION RELATED ANALYSES and* ON THE USE OF VARIOUS CORRELATION CRITERIA FOR THE VALIDATION OF SATELLITES FEM M Remedia, KK Sairajan, GS Aglietti Proceedings of IAC 2013, 0 | | |
