Articles | Volume 9, issue 1
https://doi.org/10.5194/wes-9-235-2024
https://doi.org/10.5194/wes-9-235-2024
Research article
 | 
24 Jan 2024
Research article |  | 24 Jan 2024

Developing a digital twin framework for wind tunnel testing: validation of turbulent inflow and airfoil load applications

Rishabh Mishra, Emmanuel Guilmineau, Ingrid Neunaber, and Caroline Braud

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Cited articles

Abbott, I. H. and Von Doenhoff, A. E.: Theory of wing sections: including a summary of airfoil data, Courier Corporation, New York, USA, ISBN 978-0486605869, 2012. a
Bailly, C. and Comte-Bellot, G.: Homogeneous and Isotropic Turbulence, in: Turbulence, Springer, Switzerland, ISBN 978-3-319-16159-4, pp. 129–177, 2015. a, b, c, d
Bak, C.: Airfoil Design, Springer International Publishing, Cham, https://doi.org/10.1007/978-3-030-31307-4_3, pp. 95–122, 2022. a
Batchelor, G. K. and Townsend, A. A.: Decay of isotropic turbulence in the initial period, P. Roy. Soc. Lond. A Mat., 193, 539–558, https://doi.org/10.1098/rspa.1948.0061, 1948. a, b, c, d
Blackmore, T., Batten, W., and Bahaj, A.: Inlet grid-generated turbulence for large-eddy simulations, Int. J. Comput. Fluid D., 27, 307–315, 2013. a
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Short summary
To investigate the impact of turbulence on aerodynamic forces, we first model turbulent kinetic energy decay theoretically using the Taylor length scale and employ this model to create a digital wind tunnel replica for simulating grid-generated turbulence. Experimental validation shows good alignment among theory, simulations, and experiments, paving the way for aerodynamic simulations. Finally, we successfully use the digital replica to obtain force coefficients for a 2D rotor blade section.
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