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The Institute of Theoretical and Applied Mechanics
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Original version of the author's contribution as presented on CD, page 1334, code TS.FM13-1.03 .:
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Pressure gradient turbulent boundary layers developing around a wing section
Schlatter, Philipp
The results of a DNS of the flow around a NACA4412 wing section at Rec = 400, 000 and 5◦ angle of attack are presented in this study. The high-order spectral element co [...]
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