The pressure distribution over the horizontal tail surfaces of an airplane 2
Description:
From Summary: "This investigation was undertaken to determine whether the results obtained upon model tail surfaces can be used to accurately predict loads upon the full-sized tail; and also to find the distribution of load when large elevator angles are used, as the loads from such angles can not be obtained readily in free flight. The method consisted in using a metal horizontal tail surface inside of which small air passages, connecting with a series of holes in the surface, led the pressure…
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Date:
1921
Creator:
Norton, F. H. & Bacon, D. L.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department