| Corrugated laminate homogenization model G Kress, M Winkler Composite Structures 92 (3), 795-810, 2010 | 115 | 2010 |
| Mass estimation of transport aircraft wingbox structures with a CAD/CAE-based multidisciplinary process F Hürlimann, R Kelm, M Dugas, K Oltmann, G Kress Aerospace Science and Technology 15 (4), 323-333, 2011 | 81 | 2011 |
| Optimization of segmented constrained layer damping with mathematical programming using strain energy analysis and modal data G Lepoittevin, G Kress Materials & Design 31 (1), 14-24, 2010 | 77 | 2010 |
| Corrugated laminate analysis: a generalized plane-strain problem G Kress, M Winkler Composite Structures 93 (5), 1493-1504, 2011 | 56 | 2011 |
| Model for interlaminar normal stress in singly curved laminates G Kress, R Roos, M Barbezat, C Dransfeld, P Ermanni Composite Structures 69 (4), 458-469, 2005 | 47 | 2005 |
| Deformation limits for corrugated cross-ply laminates M Winkler, G Kress Composite Structures 92 (6), 1458-1468, 2010 | 46 | 2010 |
| Enhanced model for interlaminar normal stress in singly curved laminates R Roos, G Kress, M Barbezat, P Ermanni Composite Structures 80 (3), 327-333, 2007 | 44 | 2007 |
| Shape optimization of a flywheel GR Kress Structural and Multidisciplinary Optimization 19, 74-81, 2000 | 39 | 2000 |
| Influence of corrugation geometry on the substitute stiffness matrix of corrugated laminates M Winkler, G Kress Composite Structures 94 (9), 2827-2833, 2012 | 31 | 2012 |
| A new aligned short-carbon-fiber-reinforced thermoplastic prepreg T Flemming, G Kress, M Flemming Advanced composite materials 5 (2), 151-159, 1996 | 29 | 1996 |
| Fatigue response of notched graphite/epoxy laminates GR Kress, WW Stinchcomb ASTM International, 1985 | 29 | 1985 |
| A post-processing method for interlaminar normal stresses in doubly curved laminates R Roos, G Kress, P Ermanni Composite Structures 81 (3), 463-470, 2007 | 28 | 2007 |
| Non-linear stiffness response of corrugated laminates in tensile loading C Thurnherr, L Ruppen, G Kress, P Ermanni Composite Structures 157, 244-255, 2016 | 27 | 2016 |
| Non-linear constitutive model for plain-weave composites AH Nayfeh, GR Kress Composites Part B: Engineering 28 (5-6), 627-634, 1997 | 27 | 1997 |
| Honeycomb sandwich residual stress deformation pattern G Kress, M Winkler Composite structures 89 (2), 294-302, 2009 | 26 | 2009 |
| Complex-shaped beam element and graph-based optimization of compliant mechanisms M Sauter, G Kress, M Giger, P Ermanni Structural and Multidisciplinary Optimization 36, 429-442, 2008 | 26 | 2008 |
| Mechanical response of a helical body to axial, torsional and radial strain K Nikolaos, K Gerald International Journal of Mechanical Sciences 94, 260-265, 2015 | 24 | 2015 |
| Finite element model updating of vibrating structures under free–free boundary conditions for modal damping prediction G Lepoittevin, G Kress Mechanical systems and signal processing 25 (6), 2203-2218, 2011 | 24 | 2011 |
| Stiffness reduction in laminate coupons due to the free-edge effect W Becker, G Kress Composites Science and Technology 52 (1), 109-115, 1994 | 24 | 1994 |
| Investigation of local load introduction methods in aircraft pre-design F Hürlimann, R Kelm, M Dugas, G Kress Aerospace Science and Technology 21 (1), 31-40, 2012 | 22 | 2012 |
Michael MattesTechnical University of DenmarkVerified email at elektro.dtu.dk
