Flight tests in natural icing conditions made with two 8-ft chord heated airfoils of different section; previously derived equations for calculating rate of heat transfer from airfoils in icing conditions were verified. (see also abstract in Soc Automotive Engrs -- Trans v 2 n 3 July 1948 p 369-78)
Calculation of heat required for wing thermal ice prevention in specified icing conditions
Nat Advisory Committee Aeronautics -- Tech Note
1947
107 pages
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Calculation of Heat Required for WING THERMAL ICE PREVENTION in Specified Icing Conditions
SAE Technical Papers | 1948
|Engineering Index Backfile | 1946
|Online Contents | 1994
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