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