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Abdalla M. M.
Abdalla M. M.
Correu electrònic verificat a zewailcity.edu.eg
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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
7312009
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
2842007
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
2842007
Design of variable–stiffness laminates using lamination parameters
S Setoodeh, MM Abdalla, Z Gürdal
Composites Part B: Engineering 37 (4-5), 301-309, 2006
2822006
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
2772009
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
2032010
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
2032010
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
1982010
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
1752011
Global and local buckling analysis of grid-stiffened composite panels
D Wang, MM Abdalla
Composite Structures 119, 767-776, 2015
1452015
Stiffness optimization of composite wings with aeroelastic constraints
JKS Dillinger, T Klimmek, MM Abdalla, Z Gürdal
Journal of aircraft 50 (4), 1159-1168, 2013
1412013
Mechanism for warp-controlled twist of a morphing wing
R Vos, Z Gürdal, M Abdalla
Journal of Aircraft 47 (2), 450-457, 2010
1332010
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
1302005
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
1292010
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
1102008
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
1022019
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
1022009
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
952013
Design tailoring for pressure pillowing using tow-placed steered fibers
A Alhajahmad, MM Abdalla, Z Gürdal
Journal of aircraft 45 (2), 630-640, 2008
912008
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
902010
En aquests moments el sistema no pot dur a terme l'operació. Torneu-ho a provar més tard.
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