| A three-node Mindlin plate element with improved transverse shear A Tessler, TJR Hughes Computer Methods in Applied Mechanics and Engineering 50 (1), 71-101, 1985 | 346 | 1985 |
| A least-squares variational method for full-field reconstruction of elastic deformations in shear-deformable plates and shells A Tessler, JL Spangler Computer methods in applied mechanics and engineering 194 (2-5), 327-339, 2005 | 345 | 2005 |
| A consistent refinement of first-order shear deformation theory for laminated composite and sandwich plates using improved zigzag kinematics A Tessler, M Di Sciuva, M Gherlone Journal of Mechanics of Materials and Structures 5 (2), 341-367, 2010 | 261 | 2010 |
| A refined zigzag beam theory for composite and sandwich beams A Tessler, M Di Sciuva, M Gherlone Journal of Composite Materials 43 (9), 1051-1081, 2009 | 261 | 2009 |
| On a hierarchy of conforming Timoshenko beam elements A Tessler, SB Dong Computers & structures 14 (3-4), 335-344, 1981 | 258 | 1981 |
| Shape sensing of 3D frame structures using an inverse finite element method M Gherlone, P Cerracchio, M Mattone, M Di Sciuva, A Tessler International Journal of Solids and Structures 49 (22), 3100-3112, 2012 | 237 | 2012 |
| Combined finite element and peridynamic analyses for predicting failure in a stiffened composite curved panel with a central slot E Oterkus, E Madenci, O Weckner, S Silling, P Bogert, A Tessler Composite Structures 94 (3), 839-850, 2012 | 237 | 2012 |
| A quadrilateral inverse-shell element with drilling degrees of freedom for shape sensing and structural health monitoring A Kefal, E Oterkus, A Tessler, JL Spangler Engineering science and technology, an international journal 19 (3), 1299-1313, 2016 | 230 | 2016 |
| An improved treatment of transverse shear in the Mindlin-type four-node quadrilateral element A Tessler, TJR Hughes Computer methods in applied mechanics and engineering 39 (3), 311-335, 1983 | 219 | 1983 |
| A variational principle for reconstruction of elastic deformations in shear deformable plates and shells A Tessler National Aeronautics and Space Administration, Langley Research Center, 2003 | 218 | 2003 |
| An inverse finite element method for beam shape sensing: Theoretical framework and experimental validation M Gherlone, P Cerracchio, M Mattone, M Di Sciuva, A Tessler Smart Materials and Structures 23 (4), 045027, 2014 | 193 | 2014 |
| Inverse FEM for full-field reconstruction of elastic deformations in shear deformable plates and shells A Tessler, JL Spangler 2nd European workshop on structural health monitoring, 2004 | 184 | 2004 |
| C0 beam elements based on the refined zigzag theory for multilayered composite and sandwich laminates M Gherlone, A Tessler, M Di Sciuva Composite Structures 93 (11), 2882-2894, 2011 | 151 | 2011 |
| Assessment of the refined zigzag theory for bending, vibration, and buckling of sandwich plates: a comparative study of different theories L Iurlaro, M Gherlone, M Di Sciuva, A Tessler Composite Structures 106, 777-792, 2013 | 142 | 2013 |
| An enhanced inverse finite element method for displacement and stress monitoring of multilayered composite and sandwich structures A Kefal, A Tessler, E Oterkus Composite Structures 179, 514-540, 2017 | 135 | 2017 |
| A novel approach for displacement and stress monitoring of sandwich structures based on the inverse Finite Element Method P Cerracchio, M Gherlone, M Di Sciuva, A Tessler Composite Structures 127, 69-76, 2015 | 133 | 2015 |
| Refinement of Timoshenko beam theory for composite and sandwich beams using zigzag kinematics A Tessler, M DiSciuva, M Gherlone | 130 | 2007 |
| A smoothed iFEM approach for efficient shape-sensing applications: Numerical and experimental validation on composite structures A Kefal, IE Tabrizi, M Yildiz, A Tessler Mechanical Systems and Signal Processing 152, 107486, 2021 | 120 | 2021 |
| C0 triangular elements based on the Refined Zigzag Theory for multilayer composite and sandwich plates D Versino, M Gherlone, M Mattone, M Di Sciuva, A Tessler Composites Part B: Engineering 44 (1), 218-230, 2013 | 110 | 2013 |
| An inverse interpolation method utilizing in-flight strain measurements for determining loads and structural response of aerospace vehicles S Shkarayev, R Krashantisa, A Tessler | 110 | 2004 |
Marco GherlonePolitecnico di Torino, Department of Mechanical and Aerospace Engineering在 polito.it 的电子邮件经过验证
