| A vortex lattice MATLAB implementation for linear aerodynamic wing applications T Melin Master's Thesis, Department of Aeronautics, Royal Institute of Technology …, 2000 | 283 | 2000 |
| Morphing winglets for aircraft multi-phase improvement N Ursache, T Melin, A Isikveren, M Friswell 7th AIAA ATIO Conf, 2nd CEIAT Int'l Conf on Innov and Integr in Aero …, 2007 | 59 | 2007 |
| User’s guide and reference manual for Tornado T Melin Royal Inst. of Technology (KTH), Stockholm, Sweden, 2000 | 55 | 2000 |
| Technology integration for active poly-morphing winglets development NM Ursache, T Melin, AT Isikveren, MI Friswell Smart Materials, Adaptive Structures and Intelligent Systems 43314, 775-782, 2008 | 44 | 2008 |
| TORNADO a Vortex-Lattice Matlab implementation for linear aerodynamic wing applications T Melin Royal Institute of Technology, 2000 | 32 | 2000 |
| Parametric airfoil catalog, Part II: Göttingen 673 to YS930: An aerodynamic and geometric comparison between parametrized and point cloud airfoils T Melin Linköping University Electronic Press, 2013 | 22 | 2013 |
| Parametric airfoil catalog, Part II: Göttingen 673 to YS930: An aerodynamic and geometric comparison between parametrized and point cloud airfoils T Melin Linköping University Electronic Press, 2013 | 20 | 2013 |
| Subscale flight testing used in conceptual design C Jouannet, P Berry, T Melin, K Amadori, D Lundström, I Staack Aircraft Engineering and Aerospace Technology 84 (3), 192-199, 2012 | 18 | 2012 |
| Induced-drag compressibility correction for three-dimensional vortex-lattice methods T Melin, AT Isikveren, MI Friswell Journal of Aircraft 47 (4), 1458-1460, 2010 | 18 | 2010 |
| Parametric aircraft conceptual design space I Staack, R Chaitanya Manjula, P Berry, T Melin, K Amadori, C Jouannet, ... 28th Congress of the International Council of the Aeronautical Sciences …, 2012 | 17 | 2012 |
| Glider performance analysis and intermediate-fidelity modelling of underwater vehicles C Deutsch, J Kuttenkeuler, T Melin Ocean Engineering 210, 107567, 2020 | 14 | 2020 |
| Parametric wing profile description for conceptual design T Melin, K Amadori, P Krus The International Conference of the European Aerospace societies CEAS2011, 2011 | 13 | 2011 |
| Using internet interactions in developing vortex lattice software for conceptual design T Melin Licentiate Thesis, 2003 | 12 | 2003 |
| Application of Vortex generators to a blunt body T Gustavsson, T Melin KTH Engineering Sciences, Department of Aeronautical and Vehicle Engineering …, 2006 | 11 | 2006 |
| Aircraft geometry and meshing with common language schema CPACS for variable-fidelity MDO applications M Zhang, A Jungo, AA Gastaldi, T Melin Aerospace 5 (2), 47, 2018 | 10 | 2018 |
| Tornado: a vortex lattice method implemented in MATLAB T Melin Glenn Research Center, NASA,(Last accessed 2019-02-03). https://tornado …, 2017 | 10 | 2017 |
| Knowledge-based design for future combat aircraft concepts RC Munjulury, I Staack, AM Abdalla, T Melin, C Jouannet, P Krus 29th Congress of the International Council of the Aeronautical Sciences, St …, 2014 | 10 | 2014 |
| Multidisciplinary Design in Aeronautics, Enhanced by Simulation-Experiment Synergy T Melin KTH, 2006 | 9 | 2006 |
| Tornado T Melin KTH, Stockholm, Sweden, Masters Thesis and continued development. http://www …, 2013 | 8 | 2013 |
| How industry concepts of concurrent engineering enhance aircraft design education T Melin, AT Isikveren, A Rizzi, C Stamblewski, HV Anders Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2007 | 7 | 2007 |
