Turbulent boundary layers around wing sections up to Re-c=1, 000, 000

Reynolds-number effects in the adverse-pressure-gradient (APG) turbulent boundary layer (TBL) developing on the suction side of a NACA4412 wing section are assessed in the present work. To this end, we analyze four cases at Reynolds numbers based on freestream velocity and chord length ranging from...

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Bibliographic Details
Published inThe International journal of heat and fluid flow Vol. 72; p. 86
Main Authors Vinuesa, Ricardo, Negi, Prabal Singh, Atzori, M., Hanifi, Ardeshir, Henningson, Dan S., Schlatter, Philipp
Format Journal Article
LanguageEnglish
Published 01.08.2018
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