The airfoil thickness effects on wavy leading edge phenomena at low Reynolds number regime.
Recently, the wavy leading edge airfoils, inspired by the humpback whale´s flipper, have been investigated, as flow control mechanisms, at low Reynolds numbers in order to improve aerodynamic performance in this particular flow regime. The overall aim of this work is to investigate the airfoil g...
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| Language: | English |
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Universidade de São Paulo
2016
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| Online Access: | http://www.teses.usp.br/teses/disponiveis/3/3150/tde-27092016-153422/ |