Please use this identifier to cite or link to this item: http://elea.unisa.it/xmlui/handle/10556/1859
Authors: Sergi, Vincenzo
Luchini, Paolo
Giannetti, Flavio
Abstract: The laminar-turbulent transition is a complex phenomenon involved in several multidisciplinary design issues, such as skin friction drag reduction, anti-icing and de-icing system performance prediction and heat transfer rates assessment. An accurate prediction of the boundary layer state is needed in order to control its thickness by active or passive systems. The state of the boundary layer is of high importance since skin friction drag and heat transfer rates in a turbulent boundary layer can be several times higher than those expected in laminar one. Furthermore, predicting the state of the boundary layer in wind tunnels and ensuring the same state during the real flight, by taking disturbances resulting from the experimental set up into account, leads to the design of transition triggering devices. [edited by Author]
Description: 2011 - 2012
Appears in Collections:Ingegneria meccanica

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tesi_di_dottorato_D_de_Rosa.pdftesi di dottorato806,23 kBAdobe PDFView/Open
abstract in inglese D. de Rosa.pdfabstract in inglese a cura dell'autore44,29 kBAdobe PDFView/Open
abstract in italiano D. de Rosa.pdfabstract in italiano a cura dell'autore43,79 kBAdobe PDFView/Open


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