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Latest revision as of 13:38, 14 October 2020
Abstract
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.
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Published on 01/01/2014
Volume 2014, 2014
DOI: 10.1007/978-3-319-27279-5_2
Licence: CC BY-NC-SA license
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