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Tomas Melin
Tomas Melin
FOI - The Swedish Defence Research Agency
Verified email at foi.se - Homepage
Title
Cited by
Cited by
Year
A vortex lattice MATLAB implementation for linear aerodynamic wing applications
T Melin
Royal Institute of Technology, Sweden 208, 2000
2822000
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
612007
User’s guide and reference manual for Tornado
T Melin
Royal Inst. of Technology (KTH), Stockholm, Sweden, 2000
582000
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
462008
TORNADO a Vortex-Lattice Matlab implementation for linear aerodynamic wing applications
T Melin
Royal Institute of Technology, 2000
322000
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
242013
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
222013
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
192012
Induced-drag compressibility correction for three-dimensional vortex-lattice methods
T Melin, AT Isikveren, MI Friswell
Journal of Aircraft 47 (4), 1458-1460, 2010
192010
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
162012
Glider performance analysis and intermediate-fidelity modelling of underwater vehicles
C Deutsch, J Kuttenkeuler, T Melin
Ocean Engineering 210, 107567, 2020
152020
Parametric wing profile description for conceptual design
T Melin, K Amadori, P Krus
The International Conference of the European Aerospace societies CEAS2011, 2011
132011
Using internet interactions in developing vortex lattice software for conceptual design
T Melin
Licentiate Thesis, 2003
122003
Application of Vortex generators to a blunt body
T Gustavsson, T Melin
KTH Engineering Sciences, Department of Aeronautical and Vehicle Engineering …, 2006
112006
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
102018
Tornado: a vortex lattice method implemented in MATLAB
T Melin
Glenn Research Center, NASA,(Last accessed 2019-02-03). https://tornado …, 2017
102017
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
102014
Multidisciplinary Design in Aeronautics, Enhanced by Simulation-Experiment Synergy
T Melin
KTH, 2006
92006
Tornado
T Melin
KTH, Stockholm, Sweden, Masters Thesis and continued development. http://www …, 2013
72013
Morphing winglets for aircraft multi-phase improvements, 7th AIAA Aviation Technology
NM Ursache, T Melin, AT Isikveren, MI Friswell
Integration and Operations Conference, Belfast, North Ireland, 2007
72007
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