| Surface damage evaluation of honeycomb sandwich aircraft panels using 3D scanning technology T Reyno, C Marsden, D Wowk NDT & E International 97, 11-19, 2018 | 46 | 2018 |
| An analytical study of the plasticity of sandwich honeycomb panels subjected to low-velocity impact M Sun, D Wowk, C Mechefske, IY Kim Composites Part B: Engineering 168, 121-128, 2019 | 45 | 2019 |
| An experimental and numerical investigation of core damage size in honeycomb sandwich panels subject to low-velocity impact D Wowk, T Reyno, R Yeung, C Marsden Composite Structures 254, 112739, 2020 | 34 | 2020 |
| Surface and honeycomb core damage in adhesively bonded aluminum sandwich panels subjected to low-velocity impact M Sun, D Wowk, C Mechefske, E Alexander, IY Kim Composites Part B: Engineering 230, 109506, 2022 | 32 | 2022 |
| Wing weight model for conceptual design of nonplanar configurations SA Andrews, RE Perez, D Wowk Aerospace Science and Technology 43, 51-62, 2015 | 29 | 2015 |
| Combining eddy current, thermography and laser scanning to characterize low-velocity impact damage in aerospace composite sandwich panels T Rellinger, PR Underhill, TW Krause, D Wowk Ndt & E International 120, 102421, 2021 | 22 | 2021 |
| Surface profiling and core evaluation of aluminum honeycomb sandwich aircraft panels using multi-frequency eddy current testing T Reyno, PR Underhill, TW Krause, C Marsden, D Wowk Sensors 17 (9), 2114, 2017 | 20 | 2017 |
| Development and testing of the FAST fuel performance code: Transient conditions (Part 2) A Prudil, BJ Lewis, PK Chan, JJ Baschuk, D Wowk Nuclear Engineering and Design 282, 169-177, 2015 | 19 | 2015 |
| Effect of prestrain with a path change on the strain rate sensitivity of AA5754 sheet D Wowk, K Pilkey Materials Science and Engineering: A 520 (1-2), 174-178, 2009 | 16 | 2009 |
| An adaptive remeshing technique for predicting the growth of irregular crack fronts using p-version finite element analysis D Wowk, L Alousis, PR Underhill Engineering Fracture Mechanics 207, 36-47, 2019 | 15 | 2019 |
| Characterization of low velocity impact damage in metallic honeycomb sandwich aircraft panels using finite element analysis G Clarke | 12 | 2018 |
| Influence of p-method finite element parameters on predictions of crack front geometry D Wowk, K Gamble, R Underhill Finite Elements in Analysis and Design 73, 1-10, 2013 | 11 | 2013 |
| Experimental investigation of adhesive fillet size on barely visible impact damage in metallic honeycomb sandwich panels P Kendall, M Sun, D Wowk, C Mechefske, IY Kim Composites Part B: Engineering 184, 107723, 2020 | 9 | 2020 |
| Three-dimensional modelling of interlaminar normal stresses in curved laminate components A Nagle, D Wowk, C Marsden Composite Structures 242, 112165, 2020 | 8 | 2020 |
| Effects of skin thickness and core density on the residual dent depth in aerospace sandwich panels D Wowk, C Marsden International Journal of Computational Methods and Experimental Measurements …, 2016 | 8 | 2016 |
| An experimental and numerical study of prestrained AA5754 sheet in bending D Wowk, K Pilkey Journal of Materials Processing Technology 213 (1), 1-10, 2013 | 6 | 2013 |
| A Solid Element Approach to Analyzing CANDU Fuel Element Behaviour Under Post-Dryout Heat Transfer Conditions CJ Krasnaj | 5 | 2015 |
| Effects of prestrain on the strain rate sensitivity of AA5754 sheet D Wowk, K Pilkey Canadian theses, 2008 | 5 | 2008 |
| Towards a mechanistic model for stress corrosion cracking in nuclear fuel elements A Oussoren | 4 | 2015 |
| Eddy current array inspection of damaged CFRP sandwich panels PR Underhill, T Rellinger, TW Krause, D Wowk Journal of Nondestructive Evaluation, Diagnostics and Prognostics of …, 2020 | 3 | 2020 |
