VORTEX FLOW WINGS

VORTEX FLOW WINGS

<p class="Default">The paper presents an analysis of two alternative methods of influence on integral aerodynamic characteristics at large angles of attack with global flow separation. Firstly, the approach related to flat low-profile turbulators is reviewed. Then the leading edge vo...

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Bibliographic Details
Main Authors: Eugene Udartsev, Volodymyr Rozbytskyi, Artemii Sattarov
Format: Article
Language:English
Published: National Aviation University 2018-12-01
Series:Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu
Subjects:
vortex flow wing
aerodynamic performance
post-stall angles of attack
turbulators
leading edge vortex generators
global stall, numerical modeling
Online Access:http://jrnl.nau.edu.ua/index.php/visnik/article/view/13495

Internet

http://jrnl.nau.edu.ua/index.php/visnik/article/view/13495

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