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

Name: The effect of aspect ratio and angle of attack on wing-plate junction flow
Creator: Tingyi Zhang
Published: 2019-11-01T05:53:02.556Z
Keywords: Engineering, Aerospace Engineering, Mechanical Engineering

Zhang, Tingyi; Ding, Yuchen; Awasthi, Manuj; Moreau, Danielle; Doolan, Con

doi:10.17632/b39sxdbtpx.1

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

Published: 1 November 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.

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

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