An investigation at low speed of a large-scale triangular wing of aspect ratio two I: characteristics of a wing having a double-wedge airfoil section with maximum thickness at 20-percent chord
Description: Report presenting an investigation of the low-speed characteristics of a 25-foot span triangular wing with an aspect ratio of 2. the airfoil section of the wing was a symmetrical double wedge with 5-percent maximum thickness at 20-percent chord. Results regarding the longitudinal characteristics, lateral characteristics, and directional characteristics are provided.
Date: November 13, 1947
Creator: Anderson, Adrien E.
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