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
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.
Engineering, Aerospace Engineering, Mechanical Engineering