Proceedings of the VII European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS Congress 2016) 2016
DOI: 10.7712/100016.1908.7206
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A Mesh Morphing Based Fsi Method Used in Aeronautical Optimization Applications

Abstract: In this paper a fast and efficient mesh morphing based technique to perform FSI analyses for aeroelastic design and optimization applications is presented. The procedure is based on the finite volume CFD solver (OpenFOAM® and SU2) coupled with the RBF Morph™ tool capable of deforming the surface and volume mesh of the computational domain according to the mode superposition method. Structural vibration modes of the geometry of interest are calculated in a pre-processing stage by means of a FEM solver and later… Show more

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Cited by 16 publications
(7 citation statements)
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“…On the left side, the deformed configuration for baseline is shown together with the rigid original model. A very similar approach was shown in [56], using OpenFOAM and ANSYS APDL for the optimization of the WATTsUP electric aircraft propeller, with an increase in the weighted sum of efficiencies at two different flight regimes equal to 4.0%.…”
Section: Steady Fsi Examplesmentioning
confidence: 86%
“…On the left side, the deformed configuration for baseline is shown together with the rigid original model. A very similar approach was shown in [56], using OpenFOAM and ANSYS APDL for the optimization of the WATTsUP electric aircraft propeller, with an increase in the weighted sum of efficiencies at two different flight regimes equal to 4.0%.…”
Section: Steady Fsi Examplesmentioning
confidence: 86%
“…Notable examples of RBF applications are fluid-dynamic and structural shape optimizations [14,35], fluid structure interaction [3,8], and motorsport [45], nautical [13,50], road infrastructures [48] and medical [9] analyses.…”
Section: Rbfmentioning
confidence: 99%
“…As visible, the FSI optimisation confirms that there is room for effectively optimise the winglet in cruise conditions. A similar multi-physic workflow has been implemented for the optimisation of the propeller of the Pipistrel’s electric aircraft WATTsUP (Andrejašič et al , 2016), obtaining an increase of the weighted sum of efficiencies at two different flight regimes equal to 4.0 per cent.…”
Section: Industrial Applications Of Fluid Structure Interaction Modal Approachmentioning
confidence: 99%