Open AccessTheoretical Prediction of Roll Moment Due to Sideslip for Thin Low-Aspect-Ratio Wings
Author(s) -
Thomas Linehan,
Kamran Mohseni
Publication year - 2019
Publication title -
aiaa journal
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.828
H-Index - 158
eISSN - 1081-0102
pISSN - 0001-1452
DOI - 10.2514/1.j057160
Subject(s) - mechanics , swept wing , reynolds number , angle of attack , aspect ratio (aeronautics) , chord (peer to peer) , vortex , wing , leading edge , wingtip vortices , lift (data mining) , vortex lift , flow separation , stall (fluid mechanics) , geometry , materials science , lift coefficient , physics , mathematics , aerodynamics , vorticity , turbulence , horseshoe vortex , computer science , thermodynamics , composite material , distributed computing , data mining
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