The Effect of Airfoil Thickness and Plan Form on Lateral Control
Description:
This investigation was carried out for the purpose of determining the effectiveness of ailerons and tests were made on six model airfoils in the no. 1 wind tunnel of the National Advisory Committee for Aeronautics. The method consisted in measuring the rolling moments and aileron moments in the ordinary way.The results show that the thickness of the airfoil has very little effect on either the rolling moment or the hinge moment, although the resulting efficiency is somewhat higher for the taper…
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Date:
1924
Creator:
Hoot, H. I.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department