Abstract
This chapter describes an efficient aerodynamic design optimization methodology for wings in transonic flow. The approach replaces a computationally expensive high-fidelity computational fluid dynamic model (CFD) in an iterative optimization process with a corrected polynomial approximation model constructed by a cheap low-fidelity CFD model. The output space mapping technique is used to correct the approximation model to yield an accurate predictor of the high-fidelity one. The algorithm is applied to two transonic wing design problems.
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Leifsson, L., Koziel, S., Jonsson, E. (2014). Wing Aerodynamic Shape Optimization by Space Mapping. In: Obaidat, M., Filipe, J., Kacprzyk, J., Pina, N. (eds) Simulation and Modeling Methodologies, Technologies and Applications. Advances in Intelligent Systems and Computing, vol 256. Springer, Cham. https://doi.org/10.1007/978-3-319-03581-9_23
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DOI: https://doi.org/10.1007/978-3-319-03581-9_23
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-03580-2
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