An investigation has been made of the effect of aerodynamic heating on propeller-blade temperatures. The blade temperature rise resulting from aerodynamic heating was measured and the relation between the resulting blade temperatures and the outer limit of the iced-over region was examined. It was found that the outermost station at which ice formed on a propeller blade was determined by the blade temperature rise resulting from the aerodynamic heating at that point.
The Effects of Aerodynamic Heating on Ice Formations on Airplane Propellers
1940-08-01
Miscellaneous
No indication
English
Engineering Index Backfile | 1939
|Development of airplane propellers
Engineering Index Backfile | 1949
|Making micarta airplane propellers
Engineering Index Backfile | 1929
|Bakelite-micarta airplane propellers
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