Account of investigation to determine pressure distribution over two horizontal tail surfaces in uniform free flight. n 119 1921 40 pp. 85 figs, Shows that results obtained upon model tail surfaces can be used to accurately predict loads upon full-sized tail and also to find distribution of load when large elevator angles are used. n 148 1922 26 pp. 33 figs., deals with distribution of pressure during accelerated flight of full-sized airplane, for purpose of determining magnitude of tail and fuselage stresses in stunting.
The pressure distribution over the horizontal tail surfaces of an airplane
Nat. Advisory Committee Aeronautics, report
1921
4 figs
Report
English
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Engineering Index Backfile | 1929
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