SmartBlades 2.0 Rotor Blade Nastran Models
Authors/Creators
- 1. Deutsches Zentrum für Luft- und Raumfahrt (DLR)
- 2. Delft University of Technology
Description
The SmartBlades 2.0 project was funded by the Federal Ministry for Economic Affairs and Energy (BMWi) under the Funding number: 0324032.
The reference finite element model in which this dataset is based upon consists of a validated wind turbine blade model for this 20-meters blade:
Christian Willberg. (2020). Smartblades 2 finite element reference wind turbine blade model (1.1) [Data set]. Zenodo. https://doi.org/10.5281/zenodo.4604693
This dataset includes four finite element models of the SmartBlades 2.0 Rotor Blade, described below. All input files "*.bdf" were used in MSC Nastran version 2018.2 to generate the output files "*.h5".
1) SmartBlades2 Rotor Blade Model V02 Topology Update
Willberg, C. model updated with topology features in the trailing edge, and spar-web joint regions. Including additional strucutral and test sensor masses, and refined mesh of 50mm element size.
1A) Model incorporating a clamped root boundary condition and test sensor masses:
- Input: SmartBlades2_Rotor_Blade_Nastan_Model_V02-Topology_Update-Root_Clamped.bdf
- Output: SmartBlades2_Rotor_Blade_Nastan_Model_V02-Topology_Update-Root_Clamped.h5
1B) Model incorporating a free-free boundary condition:
- Input: SmartBlades2_Rotor_Blade_Nastan_Model_V02-Topology_Update-Free_Free.bdf
- Output: SmartBlades2_Rotor_Blade_Nastan_Model_V02-Topology_Update-Free_Free.h5
2) SmartBlades2 Rotor Blade Model V02b Sparweb Free Joint Variant
The V02 Topology Update model including RBE2 connections along the spar-web joints with decoupled rotation in the spanwise axis.
2A) Model incorporating a clamped root boundary condition and test sensor masses:
- Input: SmartBlades2_Rotor_Blade_Nastan_Model_V02b-Sparweb_Free_Joint-Root_Clamped.bdf
- Output: SmartBlades2_Ro tor_Blade_Nastan_Model_V02b-Sparweb_Free_Joint-Root_Clamped.h5
2B) Model incorporating a free-free boundary condition:
- Input: SmartBlades2_Rotor_Blade_Nastan_Model_V02b-Sparweb_Free_Joint-Free_Free.bdf
- Output: SmartBlades2_Rotor_Blade_Nastan_Model_V02b-Sparweb_Free_Joint-Free_Free.h5
| Diameter of the rotor | 46.61m |
| Nominal rotational speed | 37.1 rpm |
| Length of rotor blade | 19.99 m |
| Maximum chord length | 2.38 m |
| Max. pre-bend | 1 m |
| Surface of main shell | 69.8 m² |
| Blade nominal mass |
Fiber mass (dry) 889.5 kg Infusion Resin 579.3 kg Bonding Resin 44 kg Other materials (e.g. Foam) 80.5 kg Extra masses (e.g. Sensors) 123.4 kg Total mass of the blade 17168 kg |
Files
smartblade2-connecting-the-mould-halves_29303.jpg
Files
(308.0 MB)
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Additional details
Related works
- References
- Dataset: 10.5281/zenodo.3628356 (DOI)
References
- Willberg, C. and Ravi, R. and Rieke, J. and Heinecke, F. (2021) Validation of a 20m wind turbine blade model. Energies, 14 (9). Multidisciplinary Digital Publishing Institute (MDPI). doi: 10.3390/en14092451. ISSN 1996-1073.
- Gundlach, J. and Govers, Y. (2019) Experimental modal analysis of aeroelastic tailored rotor blades in different boundary conditions. Journal of Physics: Conference Series, 1356 (012023). Institute of Physics (IOP) Publishing. doi: 10.1088/1742-6596/1356/1/012023. ISSN 1742-6588.
- Knebusch, J. and Gundlach, J. and Govers, Y. (2020) A systematic investigation of common gradient based model updating approaches applied to high-fidelity test-data of a wind turbine rotor blade. In: Proceedings of the XI International Conference on Structural Dynamics, pp. 2159-2174. EASD Procedia. EURODYN 2020 - XI International Conference on Structural Dynamics, 23.-26. Nov. 2020, Athens, Greece (Online). doi: 10.47964/1120.9175.19508. ISBN 978-618-85072-2-7. ISSN 23119020.
- Foulds, D. (2021) Validation of Breathing Modes in Wind Turbine Blade Finite Element Models. Master's Thesis, Delft University of Technology. Official URL: http://resolver.tudelft.nl/uuid:d28b47de-3229-48c4-aa79-cd04e9775e8c