| Year |
Citation |
Score |
| 2020 |
Chevalier PL, Kassapoglou C, Gürdal Z. Fatigue behavior of composite laminates with automated fiber placement induced defects- a review International Journal of Fatigue. 140: 105775. DOI: 10.1016/J.Ijfatigue.2020.105775 |
0.382 |
|
| 2019 |
Labans E, Bisagni C, Celebi M, Tatting B, Gürdal Z, Blom-Schieber A, Rassaian M, Wanthal S. Bending of Composite Cylindrical Shells with Circular Cutouts: Experimental Validation Journal of Aircraft. 56: 1534-1550. DOI: 10.2514/1.C035247 |
0.381 |
|
| 2019 |
Çelebi M, Gürdal Z, Tatting B, Blom-Schieber A, Rassaian M, Wanthal S, Türkmen HS. Bending of Composite Cylindrical Shells with Circular Cutouts: Buckling and Failure Analysis Journal of Aircraft. 56: 1551-1564. DOI: 10.2514/1.C035246 |
0.376 |
|
| 2017 |
Khani A, Abdalla MM, Gürdal Z, Sinke J, Buitenhuis A, Tooren MJLV. Design, manufacturing and testing of a fibre steered panel with a large cut-out Composite Structures. 180: 821-830. DOI: 10.1016/J.Compstruct.2017.07.086 |
0.496 |
|
| 2015 |
Khani A, Abdalla MM, Gürdal Z. Optimum tailoring of fibre-steered longitudinally stiffened cylinders Composite Structures. 122: 343-351. DOI: 10.1016/J.Compstruct.2014.11.071 |
0.541 |
|
| 2014 |
Gomes VS, Lopes CS, Pires FFA, Gürdal Z, Camanho PP. Fibre steering for shear-loaded composite panels with cutouts Journal of Composite Materials. 48: 1917-1926. DOI: 10.1177/0021998313492356 |
0.503 |
|
| 2014 |
Guo Y, Nagy AP, Gürdal Z. A layerwise theory for laminated composites in the framework of isogeometric analysis Composite Structures. 107: 447-457. DOI: 10.1016/J.Compstruct.2013.08.016 |
0.404 |
|
| 2013 |
Yao W, Chen X, Huang Y, Gurdal Z, Van Tooren M. Sequential optimization and mixed uncertainty analysis method for reliability-based optimization Aiaa Journal. 51: 2266-2277. DOI: 10.2514/1.J052327 |
0.451 |
|
| 2013 |
Dillinger J, Klimmek T, Abdalla MM, Gürdal Z. Stiffness Optimization of Composite Wings with Aeroelastic Constraints Journal of Aircraft. 50: 1159-1168. DOI: 10.2514/1.C032084 |
0.595 |
|
| 2013 |
Pahlavan L, Kassapoglou C, Gürdal Z. Spectral formulation of finite element methods using Daubechies compactly-supported wavelets for elastic wave propagation simulation Wave Motion. 50: 558-578. DOI: 10.1016/J.Wavemoti.2012.12.006 |
0.353 |
|
| 2012 |
Pahlavan L, Kassapoglou C, Suiker AA, Gürdal Z. A 2D wavelet-based spectral finite element method for elastic wave propagation Philosophical Magazine. 92: 3699-3722. DOI: 10.1080/14786435.2012.685965 |
0.303 |
|
| 2012 |
Khani A, Abdalla MM, Gürdal Z. Circumferential stiffness tailoring of general cross section cylinders for maximum buckling load with strength constraints Composite Structures. 94: 2851-2860. DOI: 10.1016/J.Compstruct.2012.04.018 |
0.504 |
|
| 2012 |
Díaz J, Fagiano C, Abdalla MM, Gürdal Z, Hernández S. A study of interlaminar stresses in variable stiffness plates Composite Structures. 94: 1192-1199. DOI: 10.1016/J.Compstruct.2011.10.016 |
0.398 |
|
| 2012 |
Campen JMJFv, Kassapoglou C, Gürdal Z. Generating realistic laminate fiber angle distributions for optimal variable stiffness laminates Composites Part B-Engineering. 43: 354-360. DOI: 10.1016/J.Compositesb.2011.10.014 |
0.499 |
|
| 2011 |
Irisarri Fc, Abdalla MM, Gürdal Z. Improved Shepard's Method for the Optimization of Composite Structures Aiaa Journal. 49: 2726-2736. DOI: 10.2514/1.J051109 |
0.35 |
|
| 2011 |
Breuker RD, Abdalla MM, Gürdal Z. A Generic Morphing Wing Analysis and Design Framework Journal of Intelligent Material Systems and Structures. 22: 1025-1039. DOI: 10.1177/1045389X11414958 |
0.425 |
|
| 2011 |
Mistry M, Gandhi F, Nagelsmit M, Gurdal Z. Actuation requirements of a warp-induced variable twist rotor blade Journal of Intelligent Material Systems and Structures. 22: 919-933. DOI: 10.1177/1045389X11404957 |
0.336 |
|
| 2011 |
Rahman T, Jansen EL, Gürdal Z. Dynamic buckling analysis of composite cylindrical shells using a finite element based perturbation method Nonlinear Dynamics. 66: 389-401. DOI: 10.1007/S11071-011-0056-9 |
0.368 |
|
| 2011 |
Nagy AP, Abdalla MM, Gürdal Z. Isogeometric design of elastic arches for maximum fundamental frequency Structural and Multidisciplinary Optimization. 43: 135-149. DOI: 10.1007/S00158-010-0549-Z |
0.536 |
|
| 2011 |
Jansen E, Rahman T, Gürdal Z. Dynamic Stability Analysis of Shells Using a Finite Element Based Reduction Method Pamm. 11: 229-230. DOI: 10.1002/Pamm.201110106 |
0.343 |
|
| 2010 |
IJsselmuiden ST, Abdalla MM, Gurdal Z. Optimization of Variable-Stiffness Panels for Maximum Buckling Load Using Lamination Parameters Aiaa Journal. 48: 134-143. DOI: 10.2514/1.42490 |
0.598 |
|
| 2010 |
Alhajahmad A, Abdalla MM, Gürdal Z. Optimal Design of Tow-Placed Fuselage Panels for Maximum Strength with Buckling Considerations Journal of Aircraft. 47: 775-782. DOI: 10.2514/1.40357 |
0.59 |
|
| 2010 |
Vos R, Gurdal Z, Abdalla M. Mechanism for Warp-Controlled Twist of a Morphing Wing Journal of Aircraft. 47: 450-457. DOI: 10.2514/1.39328 |
0.312 |
|
| 2010 |
Thuwis GAA, Abdalla MM, Gürdal Z. Optimization of a variable-stiffness skin for morphing high-lift devices Smart Materials and Structures. 19: 124010. DOI: 10.1088/0964-1726/19/12/124010 |
0.483 |
|
| 2010 |
IJsselmuiden ST, Abdalla MM, Gürdal Z. Thermomechanical Design Optimization of Variable Stiffness Composite Panels for Buckling Journal of Thermal Stresses. 33: 977-992. DOI: 10.1080/01495739.2010.510701 |
0.56 |
|
| 2010 |
Abdelal G, Abdalla M, Gurdal Z. Transient Heat Conduction of Variable Stiffness Composite Laminate Journal of Thermal Stresses. 33: 121-134. DOI: 10.1080/01495730903454579 |
0.415 |
|
| 2010 |
Fagiano C, Abdalla MM, Gürdal Z. Interlaminar stress recovery of multilayer composite shell structures for three-dimensional finite elements Finite Elements in Analysis and Design. 46: 1122-1130. DOI: 10.1016/J.Finel.2010.08.004 |
0.372 |
|
| 2010 |
Blom AW, Abdalla MM, Gürdal Z. Optimization of course locations in fiber-placed panels for general fiber angle distributions Composites Science and Technology. 70: 564-570. DOI: 10.1016/J.Compscitech.2009.12.003 |
0.429 |
|
| 2010 |
Blom AW, Stickler PB, Gürdal Z. Optimization of a composite cylinder under bending by tailoring stiffness properties in circumferential direction Composites Part B: Engineering. 41: 157-165. DOI: 10.1016/J.Compositesb.2009.10.004 |
0.526 |
|
| 2010 |
Lopes CS, Gürdal Z, Camanho PP. Tailoring for strength of composite steered-fibre panels with cutouts Composites Part a-Applied Science and Manufacturing. 41: 1760-1767. DOI: 10.1016/J.Compositesa.2010.08.011 |
0.499 |
|
| 2010 |
Nagy AP, Abdalla MM, Gürdal Z. On the variational formulation of stress constraints in isogeometric design Computer Methods in Applied Mechanics and Engineering. 199: 2687-2696. DOI: 10.1016/J.Cma.2010.05.012 |
0.505 |
|
| 2010 |
Nagy AP, Abdalla MM, Gürdal Z. Isogeometric sizing and shape optimisation of beam structures Computer Methods in Applied Mechanics and Engineering. 199: 1216-1230. DOI: 10.1016/J.Cma.2009.12.010 |
0.531 |
|
| 2010 |
Zakhama R, Abdalla MM, Gürdal Z, Smaoui H. Wind load modeling for topology optimization of continuum structures Structural and Multidisciplinary Optimization. 42: 157-164. DOI: 10.1007/S00158-010-0482-1 |
0.455 |
|
| 2010 |
Thuwis GAA, Breuker RD, Abdalla MM, Gürdal Z. Aeroelastic tailoring using lamination parameters: drag reduction of a Formula One rear wing Structural and Multidisciplinary Optimization. 41: 637-646. DOI: 10.1007/S00158-009-0437-6 |
0.336 |
|
| 2009 |
Johnson T, Frecker M, Abdalla M, Gurdal Z, Lindner D. Nonlinear analysis and optimization of diamond cell morphing wings Journal of Intelligent Material Systems and Structures. 20: 815-824. DOI: 10.1177/1045389X08098098 |
0.45 |
|
| 2009 |
Blom AW, Lopes CS, Kromwijk PJ, Gurdal Z, Camanho PP. A Theoretical Model to Study the Influence of Tow-drop Areas on the Stiffness and Strength of Variable-stiffness Laminates Journal of Composite Materials. 43: 403-425. DOI: 10.1177/0021998308097675 |
0.414 |
|
| 2009 |
Setoodeh S, Abdalla MM, IJsselmuiden ST, Gürdal Z. Design of variable-stiffness composite panels for maximum buckling load Composite Structures. 87: 109-117. DOI: 10.1016/J.Compstruct.2008.01.008 |
0.817 |
|
| 2009 |
Lopes CS, Camanho PP, Gürdal Z, Maimí P, González EV. Low-velocity impact damage on dispersed stacking sequence laminates. Part II: Numerical simulations Composites Science and Technology. 69: 937-947. DOI: 10.1016/J.Compscitech.2009.02.015 |
0.352 |
|
| 2009 |
Lopes CS, Seresta O, Coquet Y, Gürdal Z, Camanho PP, Thuis B. Low-Velocity Impact Damage On Dispersed Stacking Sequence Laminates. Part I: Experiments Composites Science and Technology. 69: 926-936. DOI: 10.1016/J.Compscitech.2009.02.009 |
0.794 |
|
| 2009 |
IJsselmuiden ST, Abdalla MM, Seresta O, Gürdal Z. Multi-step blended stacking sequence design of panel assemblies with buckling constraints Composites Part B-Engineering. 40: 329-336. DOI: 10.1016/J.Compositesb.2008.12.002 |
0.822 |
|
| 2009 |
Blom AW, Tatting BF, Hol JMAM, Gürdal Z. Fiber path definitions for elastically tailored conical shells Composites Part B-Engineering. 40: 77-84. DOI: 10.1016/J.Compositesb.2008.03.011 |
0.444 |
|
| 2008 |
Lopes CS, Remmers JJC, Gürdal Z. Influence of Porosity on the Interlaminar Shear Strength of Fibre-Metal Laminates Key Engineering Materials. 383: 35-51. DOI: 10.4028/Www.Scientific.Net/Kem.383.35 |
0.357 |
|
| 2008 |
Alhajahmad A, Abdalla MM, Gürdal Z. Design Tailoring for Pressure Pillowing Using Tow-Placed Steered Fibers Journal of Aircraft. 45: 630-640. DOI: 10.2514/1.32676 |
0.51 |
|
| 2008 |
Breuker RD, Abdalla MM, Gürdal Z. Flutter of Partially Rigid Cantilevered Two-Dimensional Plates in Axial Flow Aiaa Journal. 46: 936-946. DOI: 10.2514/1.31887 |
0.331 |
|
| 2008 |
Seresta O, Abdalla MM, Gürdal Z. Approximate Internal Load Prediction in Composite Structures with Locally Buckled Panels Journal of Aircraft. 45: 513-522. DOI: 10.2514/1.30465 |
0.802 |
|
| 2008 |
Abdalla M, Gurdal Z, Abdelal G. Thermomechanical Response of Variable Stiffness Composite Panels Journal of Thermal Stresses. 32: 187-208. DOI: 10.1080/01495730802540916 |
0.417 |
|
| 2008 |
Blom AW, Setoodeh S, Hol JMAM, Gürdal Z. Design of variable-stiffness conical shells for maximum fundamental eigenfrequency Computers & Structures. 86: 870-878. DOI: 10.1016/J.Compstruc.2007.04.020 |
0.816 |
|
| 2008 |
Lopes CS, Gürdal Z, Camanho PP. Variable-stiffness composite panels: Buckling and first-ply failure improvements over straight-fibre laminates Computers & Structures. 86: 897-907. DOI: 10.1016/J.Compstruc.2007.04.016 |
0.497 |
|
| 2008 |
Gürdal Z, Tatting BF, Wu CK. Variable stiffness composite panels : Effects of stiffness variation on the in-plane and buckling response Composites Part a-Applied Science and Manufacturing. 39: 911-922. DOI: 10.1016/J.Compositesa.2007.11.015 |
0.487 |
|
| 2008 |
Kim HA, Kennedy D, Gürdal Z. Special issue on optimization of aerospace structures Structural and Multidisciplinary Optimization. 36: 1-2. DOI: 10.1007/S00158-008-0256-1 |
0.373 |
|
| 2007 |
IJsselmuiden ST, Abdalla MM, Gürdal Z. Implementation of Strength-Based Failure Criteria in the Lamination Parameter Design Space Aiaa Journal. 46: 1826-1834. DOI: 10.2514/1.35565 |
0.514 |
|
| 2007 |
Adams DB, Watson LT, Seresta O, Gürdal Z. Global/Local Iteration for Blended Composite Laminate Panel Structure Optimization Subproblems Mechanics of Advanced Materials and Structures. 14: 139-150. DOI: 10.1080/15376490600719212 |
0.827 |
|
| 2007 |
Lopes CS, Camanho PP, Gürdal Z, Tatting BF. Progressive failure analysis of tow-placed, variable-stiffness composite panels International Journal of Solids and Structures. 44: 8493-8516. DOI: 10.1016/J.Ijsolstr.2007.06.029 |
0.45 |
|
| 2007 |
Abdalla MM, Setoodeh S, Gürdal Z. Design of variable stiffness composite panels for maximum fundamental frequency using lamination parameters Composite Structures. 81: 283-291. DOI: 10.1016/J.Compstruct.2006.08.018 |
0.818 |
|
| 2007 |
Seresta O, Gürdal Z, Adams DB, Watson LT. Optimal design of composite wing structures with blended laminates Composites Part B: Engineering. 38: 469-480. DOI: 10.1016/J.Compositesb.2006.08.005 |
0.839 |
|
| 2006 |
Seresta O, Ragon S, Abdalla MM, Gürdal Z, Lindner DK. Design of a recurve actuator for maximum energy efficiency Smart Materials and Structures. 15: 1919-1926. DOI: 10.1088/0964-1726/15/6/048 |
0.813 |
|
| 2006 |
Setoodeh S, Abdalla MM, Gürdal Z. Design of variable–stiffness laminates using lamination parameters Composites Part B-Engineering. 37: 301-309. DOI: 10.1016/J.Compositesb.2005.12.001 |
0.841 |
|
| 2006 |
Setoodeh S, Gürdal Z, Watson LT. Design of variable-stiffness composite layers using cellular automata Computer Methods in Applied Mechanics and Engineering. 195: 836-851. DOI: 10.1016/J.Cma.2005.03.005 |
0.831 |
|
| 2005 |
Gantovnik VB, Gürdal Z, Watson LT, Anderson-Cook CM. Genetic algorithm for mixed integer nonlinear programming problems using separate constraint approximations Aiaa Journal. 43: 1844-1853. DOI: 10.2514/1.4191 |
0.81 |
|
| 2005 |
Abdalla M, Frecker M, Gürdal Z, Johnson T, Lindner DK. Design of a piezoelectric actuator and compliant mechanism combination for maximum energy efficiency Smart Materials and Structures. 14: 1421-1430. DOI: 10.1088/0964-1726/14/6/035 |
0.36 |
|
| 2005 |
Abdalla MM, Reddy CK, Faris WF, Gürdal Z. Optimal design of an electrostatically actuated microbeam for maximum pull-in voltage Computers and Structures. 83: 1320-1329. DOI: 10.1016/J.Compstruc.2004.07.010 |
0.423 |
|
| 2005 |
Setoodeh S, Abdalla MM, Gürdal Z. Combined topology and fiber path design of composite layers using cellular automata Structural and Multidisciplinary Optimization. 30: 413-421. DOI: 10.1007/S00158-005-0528-Y |
0.823 |
|
| 2005 |
Missoum S, Gürdal Z, Setoodeh S. Study of a new local update scheme for cellular automata in structural design Structural and Multidisciplinary Optimization. 29: 103-112. DOI: 10.1007/S00158-004-0464-2 |
0.815 |
|
| 2004 |
Setoodeh S, Gürdal Z, Adams D, Watson LT. Pipeline implementation of cellular automata for structural design on message-passing multiprocessors Collection of Technical Papers - 10th Aiaa/Issmo Multidisciplinary Analysis and Optimization Conference. 3: 1634-1642. DOI: 10.1016/J.Mcm.2005.05.029 |
0.811 |
|
| 2004 |
Adams DB, Watson LT, Gürdal Z, Anderson-Cook CM. Genetic algorithm optimization and blending of composite laminates by locally reducing laminate thickness Advances in Engineering Software. 35: 35-43. DOI: 10.1016/J.Advengsoft.2003.09.001 |
0.577 |
|
| 2003 |
Ragon SA, Gurdal Z, Haftka RT, Tzong TJ. Bilevel Design of a Wing Structure Using Response Surfaces Journal of Aircraft. 40: 985-992. DOI: 10.2514/2.6884 |
0.486 |
|
| 2003 |
Chandrasekaran S, Ragon SA, Lindner DK, Gürdal Z, Boroyevich D. Optimization of an Aircraft Power Distribution Subsystem Journal of Aircraft. 40: 16-26. DOI: 10.2514/2.3089 |
0.494 |
|
| 2003 |
Abdalla MM, Song C, Lindner DK, Gurdal Z. Combined optimization of a recurve actuator and its drive circuit Journal of Intelligent Material Systems and Structures. 14: 275-286. DOI: 10.1177/1045389X03034689 |
0.385 |
|
| 2003 |
Adams DB, Watson LT, Gürdal Z. Optimization and blending of composite laminates using genetic algorithms with migration Mechanics of Advanced Materials and Structures. 10: 183-203. DOI: 10.1080/15376490306741 |
0.47 |
|
| 2002 |
Missoum S, Gürdal Z. Displacement-based optimization for truss structures subjected to static and dynamic constraints Aiaa Journal. 40: 154-161. DOI: 10.2514/6.1998-4793 |
0.547 |
|
| 2002 |
Soremekun G, Gürdal Z, Kassapoglou C, Toni D. Stacking Sequence Blending of Multiple Composite Laminates Using Genetic Algorithms Composite Structures. 56: 53-62. DOI: 10.1016/S0263-8223(01)00185-4 |
0.595 |
|
| 2002 |
Gu W, Gürdal Z, Missoum S. Elastoplastic truss design using a displacement based optimization Computer Methods in Applied Mechanics and Engineering. 191: 2907-2924. DOI: 10.1016/S0045-7825(02)00216-5 |
0.493 |
|
| 2002 |
Missoum S, Gürdal Z, Watson LT. A displacement based optimization method for geometrically nonlinear frame structures Structural and Multidisciplinary Optimization. 24: 195-204. DOI: 10.1007/S00158-002-0229-8 |
0.492 |
|
| 2002 |
Missoum S, Gürdal Z, Gu W. Optimization of nonlinear trusses using a displacement-based approach Structural and Multidisciplinary Optimization. 23: 214-221. DOI: 10.1007/S00158-002-0179-1 |
0.498 |
|
| 2001 |
Soremekun G, Gürdal Z, Haftka R, Watson L. Composite laminate design optimization by genetic algorithm with generalized elitist selection Computers & Structures. 79: 131-143. DOI: 10.1016/S0045-7949(00)00125-5 |
0.458 |
|
| 1999 |
Elseifi MA, Gürdal Z, Nikolaidis E. Convex/probabilistic models of uncertainties in geometric imperfections of stiffened composite panels Aiaa Journal. 37: 468-474. DOI: 10.2514/2.757 |
0.486 |
|
| 1999 |
Henderson JL, Gurdal Z, Loos AC. Combined Structural and Manufacturing Optimization of Stiffened Composite Panels Journal of Aircraft. 36: 246-254. DOI: 10.2514/2.2431 |
0.585 |
|
| 1997 |
Iyengar N, Gürdal Z. Effect of Stacking Sequence on Failure of [±45/90/0]s Quasi-Isotropic Coupons with a Hole under Compression: Journal of Thermoplastic Composite Materials. 10: 136-150. DOI: 10.1177/089270579701000203 |
0.344 |
|
| 1997 |
Perry CA, Gürdal Z, Starnes JH. Minimum-Weight Design Of Compressively Loaded Stiffened Panels For Postbuckling Response Engineering Optimization. 28: 175-197. DOI: 10.1080/03052159708941131 |
0.519 |
|
| 1997 |
Tatting BF, Gürdal Z, Vasiliev VV. The brazier effect for finite length composite cylinders under bending International Journal of Solids and Structures. 34: 1419-1440. DOI: 10.1016/S0020-7683(96)00094-7 |
0.378 |
|
| 1996 |
Tatting BF, Gurdal Z, Vasiliev VV. Nonlinear response of long orthotropic tubes under bending including the Brazier effect Aiaa Journal. 34: 1934-1940. DOI: 10.2514/3.13328 |
0.37 |
|
| 1996 |
Nagendra S, Jestin D, Gürdal Z, Haftka R, Watson L. Improved genetic algorithm for the design of stiffened composite panels Computers & Structures. 58: 543-555. DOI: 10.1016/0045-7949(95)00160-I |
0.526 |
|
| 1995 |
Lee J, Gurdal Z, Griffin OH. Postbuckling of laminated composites with delaminations Aiaa Journal. 33: 1963-1970. DOI: 10.2514/3.12752 |
0.453 |
|
| 1995 |
Lee J, Griffin OH, Gürdal Z. Buckling And Postbuckling Of Circular Plates Containing Concentric Penny-Shaped Delaminations Computers & Structures. 56: 1053-1063. DOI: 10.1016/0045-7949(94)00372-A |
0.443 |
|
| 1995 |
Ley RP, Gurdal Z, Johnson ER. Optimal design of imperfect, anisotropic, ring-stiffened cylinders under combined loads Structural Optimization. 9: 160-167. DOI: 10.1007/Bf01743965 |
0.5 |
|
| 1994 |
Gurdal Z, Grall B. Buckling analysis of geodesically stiffened composite panels with discrete stiffeners Journal of Aircraft. 31: 1197-1204. DOI: 10.2514/3.46630 |
0.42 |
|
| 1994 |
Ley RP, Johnson ER, Gurdal Z. Buckling of imperfect, anisotropic, ring-stiffened cylinders under combined loads Aiaa Journal. 32: 1302-1309. DOI: 10.2514/3.12133 |
0.394 |
|
| 1994 |
Kogiso N, Watson L, Gürdal Z, Haftka R, Nagendra S. DESIGN OF COMPOSITE LAMINATES BY A GENETIC ALGORITHM WITH MEMORY Mechanics of Advanced Materials and Structures. 1: 95-117. DOI: 10.1080/10759419408945823 |
0.511 |
|
| 1994 |
Nagendra S, Gürdal Z, Haftka RT, Starnes JH. Buckling and failure characteristics of compression-loaded stiffened composite panels with a hole Composite Structures. 28: 1-17. DOI: 10.1016/0263-8223(94)90002-7 |
0.468 |
|
| 1994 |
Kogiso N, Watson LT, Gürdal Z, Haftka RT. Genetic algorithms with local improvement for composite laminate design Structural Optimization. 7: 207-218. DOI: 10.1007/Bf01743714 |
0.541 |
|
| 1994 |
Yates K, Gürdal Z, Thangjitham S. Multilevel optimization of space trusses using continuum modelling Structural Optimization. 7: 176-183. DOI: 10.1007/Bf01742464 |
0.428 |
|
| 1993 |
Gurdal Z, Olmedo R. In-plane response of laminates with spatially varying fiber orientations - Variable stiffness concept Aiaa Journal. 31: 751-758. DOI: 10.2514/3.11613 |
0.429 |
|
| 1993 |
Breivik NL, Gurdal Z, Griffin OH. Compression of laminated composite beams with initial damage Journal of Reinforced Plastics and Composites. 12: 813-824. DOI: 10.1177/073168449301200707 |
0.331 |
|
| 1993 |
Gürdal Z, Gendron G. Optimal design of geodesically stiffened composite cylindrical shells Composites Engineering. 3: 1131-1147. DOI: 10.1016/0961-9526(93)90070-Z |
0.6 |
|
| 1993 |
Shin DK, Griffin OH, Gürdal Z. Postbuckling response of laminated plates under uniaxial compression International Journal of Non-Linear Mechanics. 28: 95-115. DOI: 10.1016/0020-7462(93)90009-A |
0.378 |
|
| 1992 |
Lee J, Gurdal Z, Griffin OH. Layer-wise approach for the bifurcation problem in laminated composites with delaminations Aiaa Journal. 31: 331-338. DOI: 10.2514/3.11672 |
0.371 |
|
| 1992 |
Nagendra S, Haftka RT, Gurdal Z. Stacking sequence optimization of simply supported laminates with stability and strain constraints Aiaa Journal. 30: 2132-2137. DOI: 10.2514/3.11191 |
0.494 |
|
| 1991 |
Nagendra S, Haftka RT, Gürdal Z, Starnes JH. Design of a blade-stiffened composite panel with a hole Composite Structures. 18: 195-219. DOI: 10.1016/0263-8223(91)90033-U |
0.551 |
|
| 1990 |
Swanson GD, Gurdal Z, Starnes JH. Structural efficiency study of graphite-epoxy aircraft rib structures Journal of Aircraft. 27: 1011-1020. DOI: 10.2514/3.45975 |
0.491 |
|
| 1990 |
Gurdal Z, Young RD. Importance of anisotropy on design of compression-loaded composite corrugated panels Journal of Aircraft. 27: 378-380. DOI: 10.2514/3.25283 |
0.516 |
|
| 1990 |
Sevart JL, Griffin OH, Gürdal Z, Warner GA. Flammability and Toxicity of Composite Materials for Marine Vehicles Naval Engineers Journal. 102: 45-53. DOI: 10.1111/J.1559-3584.1990.Tb00899.X |
0.324 |
|
| 1990 |
Shin DK, GÜrdal Z, Griffin OH. A Penalty approach for nonlinear optimization with discrete design variables Engineering Optimization. 16: 29-42. DOI: 10.1080/03052159008941163 |
0.473 |
|
| 1989 |
Pindera M, Gurdal Z, Herakovich CT, Hidde JS, Starbuck JM. Mechanical Response of Aramid/Epoxy under Tensile, Compressive and Shear Loading Journal of Reinforced Plastics and Composites. 8: 410-420. DOI: 10.1177/073168448900800406 |
0.353 |
|
| 1988 |
Grossman B, Gurdal Z, Haftka RT, Strauch GJ, Eppard WM. Integrated aerodynamic/structural design of a sailplane wing Journal of Aircraft. 25: 855-860. DOI: 10.2514/3.45670 |
0.54 |
|
| 1988 |
Gurdal Z, Haftka RT. Automated design of composite plates for improved damage tolerance Astm Special Technical Publications. 5-22. DOI: 10.1520/Stp26125S |
0.491 |
|
| 1987 |
Gürdal Z, Herakovich CT. Effect of initial flaw shape on crack extension in orthotropic composite materials Theoretical and Applied Fracture Mechanics. 8: 59-75. DOI: 10.1016/0167-8442(87)90019-X |
0.305 |
|
| 1985 |
Gurdal Z, Haftka RT. Sensitivity derivatives for static test loading boundary conditions Aiaa Journal. 23: 159-160. DOI: 10.2514/3.8888 |
0.303 |
|
| 1985 |
Gürdal Z, Haftka R, Starnes J. The effect of slots on the buckling and postbuckling behavior of laminated plates Journal of Composites Technology & Research. 7: 82-87. DOI: 10.1520/Ctr10302J |
0.325 |
|
| 1985 |
Gürdal Z, Haftka RT. Design of stiffened composite panels with a fracture constraint Computers & Structures. 20: 457-465. DOI: 10.1016/0045-7949(85)90094-X |
0.501 |
|
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