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Additional design charts relating to the stalling of tapered wings

Sidney M Harmon

Abstract

Oharts are presented to show the effects of taper ratio, thickness ratio, aspeot ratio, and Reynolds number on the spanwlse location of the Initial wing stall and on ""the maxlmun lift coeffloiant of the wing.These stall " charts supplement the charts given in HACA Report Ho. 703 by including additional taper ratios and a root thickness " ratio of 0.24 tapering to 0.09 at the tip.Yor a root thickness ratio of 0.24, the effect of increasing the aspect ratio to 18 is Investigated..-..

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Key concepts: Stall (fluid mechanics), Engineering drawing, Engineering, Computer science, Aerospace engineering