| Fragility analysis of a 5-MW NREL wind turbine considering aero-elastic and seismic interaction using finite element method MA Asareh, W Schonberg, J Volz Finite Elements in Analysis and Design 120, 57-67, 2016 | 96 | 2016 |
| Effects of seismic and aerodynamic load interaction on structural dynamic response of multi-megawatt utility scale horizontal axis wind turbines MA Asareh, W Schonberg, J Volz Renewable energy 86, 49-58, 2016 | 80 | 2016 |
| Penetration and ricochet phenomena in oblique hypervelocity impact WP Schonberg, RA Taylor AIAA journal 27 (5), 639-646, 1989 | 68 | 1989 |
| Hypervelocity impact physics WP Schonberg, AJ Bean, K Darzi NASA, 1991 | 65 | 1991 |
| Hypervelocity impact response of honeycomb sandwich panels W Schonberg, F Schäfer, R Putzar Acta Astronautica 66 (3-4), 455-466, 2010 | 62 | 2010 |
| Protecting Earth-orbiting spacecraft against micro-meteoroid/orbital debris impact damage using composite structural systems and materials: An overview WP Schonberg Advances in Space Research 45 (6), 709-720, 2010 | 59 | 2010 |
| Protecting spacecraft against orbital debris impact damage using composite materials WP Schonberg Composites Part A: Applied Science and Manufacturing 31 (8), 869-878, 2000 | 59 | 2000 |
| Hypervelocity impact response of spaced composite material structures WP Schonberg International Journal of Impact Engineering 10 (1-4), 509-523, 1990 | 57 | 1990 |
| Low velocity impact of transversely isotropic beams and plates WP Schonberg, LM Keer, TK Woo International journal of solids and structures 23 (7), 871-896, 1987 | 49 | 1987 |
| Characterizing secondary debris impact ejecta WP Schonberg International Journal of Impact Engineering 26 (1-10), 713-724, 2001 | 46 | 2001 |
| Empirical hole size and crack length models for dual-wall systems under hypervelocity projectile impact WP Schonberg, JE Williamsen International Journal of Impact Engineering 20 (6-10), 711-722, 1997 | 44 | 1997 |
| Studies of hypervelocity impact phenomena as applied to the protection of spacecraft operating in the MMOD environment WP Schonberg Procedia Engineering 204, 4-42, 2017 | 43 | 2017 |
| Spacecraft wall design for increased protection against penetration by orbital debris impacts WP Schonberg, RJ Tullos AIAA journal 29 (12), 2207-2214, 1991 | 42 | 1991 |
| Smooth indentation of an isotropic cantilever beam LM Keer, WP Schonberg International journal of solids and structures 22 (1), 87-106, 1986 | 39 | 1986 |
| Hypervelocity impact penetration phenomena in aluminum space structures WP Schonberg Journal of Aerospace Engineering 3 (3), 173-185, 1990 | 38 | 1990 |
| Modelling oblique hypervelocity impact phenomena using elementary shock physics WP Schonberg, AR Ebrahim International journal of impact engineering 23 (1), 823-834, 1999 | 35 | 1999 |
| Use of composite materials in multi-wall structures to prevent perforation by hypervelocity particle impact WP Schonberg, EJ Walker Composite structures 19 (1), 15-40, 1991 | 33 | 1991 |
| Ballistic limit curves for non-spherical projectiles impacting dual-wall spacecraft systems K Hu, WP Schonberg Elsevier 29 (1 thru 10), 345, 2003 | 30 | 2003 |
| RCS-based ballistic limit curves for non-spherical projectiles impacting dual-wall spacecraft systems WP Schonberg, JE Williamsen International journal of impact engineering 33 (1-12), 763-770, 2006 | 29 | 2006 |
| Static and dynamic finite element analysis of honeycomb sandwich structures MH Triplett The University of Alabama in Huntsville, 1995 | 28 | 1995 |
Jason BairdAssociate Professor of Mining Engineering, MIssouri S&T, Loki IncorporatedVerified email at lokiconsult.com
