| High-order energy balance method to nonlinear oscillators S Durmaz, MO Kaya Journal of Applied Mathematics 2012, 2012 | 39 | 2012 |
| Approximate solutions for nonlinear oscillation of a mass attached to a stretched elastic wire S Durmaz, SA Demirbağ, MO Kaya Computers & Mathematics with Applications 61 (3), 578-585, 2011 | 30 | 2011 |
| Free vibration analysis of composite aircraft wings modeled as thin-walled beams with NACA airfoil sections S Eken Thin-Walled Structures 139, 362-371, 2019 | 26 | 2019 |
| Flexural-torsional coupled vibration of anisotropic thin-walled beams with biconvex cross-section S Eken, MO Kaya Thin-Walled Structures 94, 372-383, 2015 | 18 | 2015 |
| He's Variational Approach to Multiple Coupled Nonlinear Oscillators MO Kaya, S Durmaz, SA Demirbag International Journal of Nonlinear Sciences and Numerical Simulation 11 (10 …, 2010 | 16 | 2010 |
| Computational model for woven fabrics subjected to ballistic impact by a spherical projectile S Eken, L PHOENIX, K YAVUZ Proceedings of the American Society for Composites: Thirty-First Technical …, 2016 | 10 | 2016 |
| The Ballistic Impact Response of Flexible Composite Body Armor K YAVUZ, L PHOENIX, S EKEN Proceedings of the American Society for Composites: Thirty-First Technical …, 2016 | 8 | 2016 |
| The Ballistic Impact Response of Flexible Composite Body Armor K YAVUZ, L PHOENIX, S EKEN Proceedings of the American Society for Composites: Thirty-First Technical …, 2016 | 8 | 2016 |
| Dynamic instability of spinning launch vehicles modeled as thin-walled composite beams M Cihan, S Eken, MO Kaya Acta Mechanica 228, 4353-4367, 2017 | 6 | 2017 |
| Dynamic instability of spinning launch vehicles modeled as thin-walled composite beams M Cihan, S Eken, MO Kaya Acta Mechanica 228, 4353-4367, 2017 | 6 | 2017 |
| Active Vibration Control of Aircraft Wings Modeled as Thin-Walled Composite Beams Using Piezoelectric Actuation K Yildiz, S Eken, MO Kaya ASME International Mechanical Engineering Congress and Exposition 46483 …, 2014 | 6 | 2014 |
| Active Vibration Control of Aircraft Wings Modeled as Thin-Walled Composite Beams Using Piezoelectric Actuation K Yildiz, S Eken, MO Kaya ASME International Mechanical Engineering Congress and Exposition 46483 …, 2014 | 6 | 2014 |
| PC-Based Numerical Modeling of Ballistic Impact into Nonwoven Fibrous Targets SL Phoenix, S Eken, AK Yavuz American Society for Composites 31 Technical Conference and ASTM Committee …, 2016 | 5 | 2016 |
| Longitudinal dynamics analysis of Boeing 747-400 K Koşar, S Durmaz, EM Jafarov Proceedings of the 9th WSEAS international conference on Automatic control …, 2007 | 5 | 2007 |
| The effect of sweep angle on the limit cycle oscillations of aircraft wings S Eken, MO Kaya Advances in aircraft and spacecraft science 2 (2), 199, 2015 | 4 | 2015 |
| The effect of sweep angle on the limit cycle oscillations of aircraft wings S Eken, MO Kaya Advances in aircraft and spacecraft science 2 (2), 199, 2015 | 4 | 2015 |
| Hamiltonian approach to multiple coupled nonlinear oscillators S Durmaz, S Altay Demirbag, M Kaya Acta Physica Polonica A 121 (1), 47-49, 2012 | 4 | 2012 |
| Free vibration of an anisotropic thin-walled box beam under bending-torsion coupling S Durmaz, MO Kaya Proceedings of 3rd International Conference On Integrity, Reliability and …, 2009 | 4 | 2009 |
| Longitudinal displacement autopilot design for Boeing 747-400 by root-locus K Koşar, S Durmaz, EM Jafarov Proceedings of the 9th WSEAS international conference on Automatic control …, 2007 | 4 | 2007 |
| Coupled Bending–Torsional Dynamic Behavior of a Cantilever Beam Carrying Multiple Point Masses AK Aksongur, S Eken, MO Kaya International Journal of Mechanical Engineering and Robotics Research 8 (3 …, 2019 | 3 | 2019 |
