Computational methods for bird strike simulations: A review S Heimbs Computers & Structures 89 (23-24), 2093-2112, 2011 | 313 | 2011 |
Low velocity impact on CFRP plates with compressive preload: test and modelling S Heimbs, S Heller, P Middendorf, F Hähnel, J Weiße International Journal of Impact Engineering 36 (10-11), 1182-1193, 2009 | 262 | 2009 |
Sandwich structures with textile-reinforced composite foldcores under impact loads S Heimbs, J Cichosz, M Klaus, S Kilchert, AF Johnson Composite structures 92 (6), 1485-1497, 2010 | 243 | 2010 |
Virtual testing of sandwich core structures using dynamic finite element simulations S Heimbs Computational Materials Science 45 (2), 205-216, 2009 | 196 | 2009 |
Failure behaviour of honeycomb sandwich corner joints and inserts S Heimbs, M Pein Composite Structures 89 (4), 575-588, 2009 | 147 | 2009 |
Experimental and numerical analysis of composite folded sandwich core structures under compression S Heimbs, P Middendorf, S Kilchert, AF Johnson, M Maier Applied Composite Materials 14, 363-377, 2007 | 142 | 2007 |
Strain rate effects in phenolic composites and phenolic-impregnated honeycomb structures S Heimbs, S Schmeer, P Middendorf, M Maier Composites Science and Technology 67 (13), 2827-2837, 2007 | 115 | 2007 |
Foldcore sandwich structures and their impact behaviour: an overview S Heimbs Dynamic failure of composite and sandwich structures, 491-544, 2012 | 112 | 2012 |
Failure behaviour of composite T-joints with novel metallic arrow-pin reinforcement S Heimbs, AC Nogueira, E Hombergsmeier, M May, J Wolfrum Composite Structures 110, 16-28, 2014 | 111 | 2014 |
High velocity impact on preloaded composite plates S Heimbs, T Bergmann, D Schueler, N Toso-Pentecôte Composite Structures 111, 158-168, 2014 | 103 | 2014 |
Static and dynamic failure behaviour of bolted joints in carbon fibre composites S Heimbs, S Schmeer, J Blaurock, S Steeger Composites Part A: Applied Science and Manufacturing 47, 91-101, 2013 | 93 | 2013 |
High‐velocity impact behaviour of prestressed composite plates under bird strike loading S Heimbs, T Bergmann International Journal of Aerospace Engineering 2012 (1), 372167, 2012 | 74 | 2012 |
Aircraft sandwich structures with folded core under impact load S Heimbs, P Middendorf, C Hampf, F Hähnel, K Wolf Proc. of the 8th International Conference on Sandwich Structures, ICSS8 …, 2008 | 73 | 2008 |
Crash simulation of an F1 racing car front impact structure S Heimbs, F Strobl, P Middendorf, S Gardner, B Eddington, J Key 7th European LS-DYNA conference, 1-8, 2009 | 62 | 2009 |
Mechanical properties and energy absorption capability of woven fabric composites under±45 off-axis tension T Bergmann, S Heimbs, M Maier Composite Structures 125, 362-373, 2015 | 61 | 2015 |
Simulation of low velocity impact on composite plates with compressive preload S Heimbs, S Heller, P Middendorf Proceedings of The 7th German LS-DYNA Forum, 2008 | 60 | 2008 |
Dynamic testing and modelling of composite fuselage frames and fasteners for aircraft crash simulations S Heimbs, M Hoffmann, M Waimer, S Schmeer, J Blaurock International Journal of Crashworthiness 18 (4), 406-422, 2013 | 59 | 2013 |
Honeycomb sandwich material modeling for dynamic simulations of aircraft interior components S Heimbs, P Middendorf, M Maier 9th International LS-DYNA users conference 20, 1-13, 2006 | 56 | 2006 |
Composite crash absorber for aircraft fuselage applications S Heimbs, F Strobl, P Middendorf, JM Guimard WIT Transactions on the built environment 113, 3-14, 2010 | 55 | 2010 |
Bird strike simulations on composite aircraft structures S Heimbs SIMULIA Customer Conference, Barcelona, 73-86, 2011 | 54 | 2011 |