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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Published in | The International journal of heat and fluid flow Vol. 72; p. 86 |
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Main Authors | , , , , , |
Format | Journal Article |
Language | English |
Published |
01.08.2018
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Subjects | |
Online Access | Get full text |
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