This work presents the design of a folded Krüger device under realistic geometrical requirements for a wing with hybrid laminar flow control (HLFC). A focus is laid on the investigation of the trade-off between space allocation of the retracted Krüger and the aerodynamic high-lift performance. The results reveal that the Krüger device is able to replace a reference slat device in relation to its aerodynamic high-lift performance. Further on the reduction of the allocation space influences the high-lift performance unfavorably.
CITATION STYLE
Franke, D. M., & Wild, J. (2016). Aerodynamic design of a folded krüger device for a HLFC wing. In Notes on Numerical Fluid Mechanics and Multidisciplinary Design (Vol. 132, pp. 17–27). Springer Verlag. https://doi.org/10.1007/978-3-319-27279-5_2
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