| Celebrating the 100th anniversary of the Stoney equation for film stress: Developments from polycrystalline steel strips to single crystal silicon wafers GCAM Janssen, MM Abdalla, F Van Keulen, BR Pujada, B Van Venrooy Thin Solid Films 517 (6), 1858-1867, 2009 | 773 | 2009 |
| Design of variable-stiffness composite panels for maximum buckling load S Setoodeh, MM Abdalla, ST IJsselmuiden, Z Gürdal Composite structures 87 (1), 109-117, 2009 | 298 | 2009 |
| Design of variable stiffness composite panels for maximum fundamental frequency using lamination parameters MM Abdalla, S Setoodeh, Z Gürdal Composite structures 81 (2), 283-291, 2007 | 295 | 2007 |
| Design of variable–stiffness laminates using lamination parameters S Setoodeh, MM Abdalla, Z Gürdal Composites Part B: Engineering 37 (4-5), 301-309, 2006 | 292 | 2006 |
| Optimization of variable-stiffness panels for maximum buckling load using lamination parameters ST IJsselmuiden, MM Abdalla, Z Gurdal AIAA journal 48 (1), 134-143, 2010 | 214 | 2010 |
| Isogeometric sizing and shape optimisation of beam structures AP Nagy, MM Abdalla, Z Gürdal Computer Methods in Applied Mechanics and Engineering 199 (17-20), 1216-1230, 2010 | 211 | 2010 |
| Design of variable stiffness panels for maximum strength using lamination parameters A Khani, ST IJsselmuiden, MM Abdalla, Z Gürdal Composites Part B: Engineering 42 (3), 546-552, 2011 | 186 | 2011 |
| Global and local buckling analysis of grid-stiffened composite panels D Wang, MM Abdalla Composite Structures 119, 767-776, 2015 | 159 | 2015 |
| Stiffness optimization of composite wings with aeroelastic constraints JKS Dillinger, T Klimmek, MM Abdalla, Z Gürdal Journal of aircraft 50 (4), 1159-1168, 2013 | 153 | 2013 |
| Mechanism for warp-controlled twist of a morphing wing R Vos, Z Gürdal, M Abdalla Journal of Aircraft 47 (2), 450-457, 2010 | 143 | 2010 |
| Combined topology and fiber path design of composite layers using cellular automata S Setoodeh, MM Abdalla, Z Gürdal Structural and Multidisciplinary Optimization 30, 413-421, 2005 | 135 | 2005 |
| Optimization of course locations in fiber-placed panels for general fiber angle distributions AW Blom, MM Abdalla, Z Gürdal Composites Science and Technology 70 (4), 564-570, 2010 | 134 | 2010 |
| Implementation of strength-based failure criteria in the lamination parameter design space ST IJsselmuiden, MM Abdalla, Z Gürdal AIAA journal 46 (7), 1826-1834, 2008 | 121 | 2008 |
| Streamline stiffener path optimization (SSPO) for embedded stiffener layout design of non-uniform curved grid-stiffened composite (NCGC) structures D Wang, MM Abdalla, ZP Wang, Z Su Computer Methods in Applied Mechanics and Engineering 344, 1021-1050, 2019 | 119 | 2019 |
| Multi-step blended stacking sequence design of panel assemblies with buckling constraints ST IJsselmuiden, MM Abdalla, O Seresta, Z Gürdal Composites part b: engineering 40 (4), 329-336, 2009 | 107 | 2009 |
| Buckling optimization design of curved stiffeners for grid-stiffened composite structures D Wang, MM Abdalla, W Zhang Composite Structures 159, 656-666, 2017 | 101 | 2017 |
| Isogeometric design of anisotropic shells: optimal form and material distribution AP Nagy, ST IJsselmuiden, MM Abdalla Computer Methods in Applied Mechanics and Engineering 264, 145-162, 2013 | 99 | 2013 |
| Stacking sequence optimisation of variable stiffness laminates with manufacturing constraints DMJ Peeters, S Hesse, MM Abdalla Composite Structures 125, 596-604, 2015 | 98 | 2015 |
| Optimal design of tow-placed fuselage panels for maximum strength with buckling considerations A Alhajahmad, MM Abdalla, Z Gürdal Journal of Aircraft 47 (3), 775-782, 2010 | 95 | 2010 |
| Design tailoring for pressure pillowing using tow-placed steered fibers A Alhajahmad, MM Abdalla, Z Gürdal Journal of aircraft 45 (2), 630-640, 2008 | 93 | 2008 |
Martin RuessUniversity of Applied Sciences DüsseldorfVerified email at mytum.de
