The effect of aspect ratio and angle of attack on wing-plate junction flow

Published: 01-11-2019| Version 1 | DOI: 10.17632/b39sxdbtpx.1
Contributors:
Tingyi Zhang,
Yuchen Ding,
Manuj Awasthi,
Danielle Moreau,
Con Doolan

Description

The mean pressure of the flow field formed within wing-body junctions are presented. Wings formed from constant-chord, NACA 0012 airfoil sections were used, with aspect ratios of 0.2 and 1.0 and angles of attack of 0, 5 and 10 degree.

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