| Flexible skins for morphing aircraft using cellular honeycomb cores KR Olympio, F Gandhi Journal of intelligent material systems and structures 21 (17), 1719-1735, 2010 | 249 | 2010 |
| Zero Poisson’s ratio cellular honeycombs for flex skins undergoing one-dimensional morphing KR Olympio, F Gandhi Journal of intelligent material systems and structures 21 (17), 1737-1753, 2010 | 233 | 2010 |
| Zero-v cellular honeycomb flexible skins for one-dimensional wing morphing K Olympio, F Gandhi 48th AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials …, 2007 | 108 | 2007 |
| Design of a flexible skin for a shear morphing wing KR Olympio, F Gandhi, L Asheghian, J Kudva Journal of intelligent material systems and structures 21 (17), 1755-1770, 2010 | 75 | 2010 |
| Design of a passive flexible skin for morphing aircraft structures KR Olympio Pennsylvania State University, 2006 | 24 | 2006 |
| Evaluation of earth observation solutions for Namibia’s SDG monitoring system V Mariathasan, E Bezuidenhoudt, KR Olympio Remote Sensing 11 (13), 1612, 2019 | 23 | 2019 |
| Skin designs using multi-objective topology optimization K Olympio, F Gandhi 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2008 | 22 | 2008 |
| Optimal Cellular Core Topologies for One-Dimensional Morphing Aircraft Structures KR Olympio, F Gandhi Journal of Mechanical Design 134 (8), 081005, 2012 | 19 | 2012 |
| Holographic interferometry based on photorefractive crystal to measure 3D thermo-elastic distortion of composite structures and comparison with finite element models C Thizy, F Eliot, D Ballhause, KR Olympio, R Kluge, A Shannon, ... Optical Measurement Systems for Industrial Inspection VIII 8788, 43-54, 2013 | 10 | 2013 |
| Modeling and Numerical Analyses of Skin Design Concepts KR Olympio, F Gandhi AIAA Proceedings.[np]. 04-07 May, 2009 | 10 | 2009 |
| Compliant load-bearing skins and structures for morphing aircraft applications KR Olympio THE PENNSYLVANIA STATE UNIVERSITY, 2009 | 9 | 2009 |
| A honeycomb-based piezoelectric actuator for a flapping wing MAV KR Olympio, G Poulin-Vittrant Active and Passive Smart Structures and Integrated Systems 2011 7977, 667-682, 2011 | 7 | 2011 |
| Compliant frame: a new paradigm to enable reconfigurable aircraft structures GA Lesieutre, MI Frecker, FS Gandhi, D Ramrakhyani, S Bharti, J Browne, ... Pennsylvania State University, 2007 | 5 | 2007 |
| Design of flexible skins for morphing aircraft structures using honeycomb cores KR Olympio, F Gandhi Proc. of 47th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and …, 2006 | 5 | 2006 |
| Structural vibration tests: Use of artificial neural networks for live prediction of structural stress L Wilmes, R Olympio, KM de Payrebrune, M Schatz Applied Sciences 10 (23), 8542, 2020 | 4 | 2020 |
| Development of Bio-Mimetic Morphing Skins for Micro-UAVs L Asheghian, J Kudva, KR Olympio, F Gandhi 11th Pan-American Congress of Applied Mechanics, 2009 | 3 | 2009 |
| Piezoelectric actuation of a flapping wing accounting for nonlinear damping KR Olympio, G Poulin-Vittrant Active and Passive Smart Structures and Integrated Systems 2011 7977, 645-656, 2011 | 2 | 2011 |
| Comparison of mass operator methods considering test uncertainties KR Olympio, F Blender, M Holz, A Kommer, R Vetter Advances in Aircraft and Spacecraft Science 5 (2), 277-294, 2018 | 1 | 2018 |
| Recent advances in the negative refraction of longitudinal waves in an elastic phononic crystal AC Hladky-Hennion, C Croënne, KR Olympio, J Vasseur, B Dubus, ... 2011 IEEE International Ultrasonics Symposium, 1316-1319, 2011 | 1 | 2011 |
| Implementation and test of a robust mass operator tool KR Olympio, F Blender, M Holz, A Kommer, R Vetter 14th European Conference on Spacecraft Structures, Material and …, 2016 | | 2016 |
