Conference Proceedings
DNS of a compliant trailing edge flow
SC Schlanderer, RD Sandberg
19th AIAA/CEAS Aeroacoustics Conf. | American Institute of Aeronautics and Astronautics | Published : 2013
DOI: 10.2514/6.2013-2013
Abstract
Direct numerical simulations (DNS) of boundary layers convecting over a compliant trailing edge are considered in this study. To that end a fully coupled fluid structure interaction framework was developed by coupling a newly developed structural solver to a well validated DNS code. The moving boundaries were represented by an immersed boundary technique using feedback-forcing which was validated with laminar boundary layer instability growth rates and a trailing edge noise problem. First results indicate that the compliant trailing edge yields a decreased noise level in the low and intermediate frequency range. In contrast to that an increased sound level has been found in frequency ranges ..
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