Analysis of low Reynolds number flow past Gurney flap

The trailing edge region of a single element wing fitted with Gurney flap at low Reynoldsnumbers has been studied.The complex flow separation phenomena on airfoils with Gurney flap at low Reynolds numbershave some specific features as the separation on set and reattachment locations and the streamli...

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Bibliographic Details
Main Authors: Ion MĂLĂEL, Horia DUMITRESCU
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2010-12-01
Series:INCAS Bulletin
Subjects:
Online Access:http://bulletin.incas.ro/files/horia_dumitrescu_v2no4_full.pdf