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Effect Of Ice And Heated-Air Deicing On The Aerodynamic Performance Of Propellers

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Corson, Blake W., author.
Conference Name:
SAE NATIONAL AERONAUTIC AND AIR TRANSPORT MEETING
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1948
Summary:
SUMMARYA review is made of several wind-tunnel investigations dealing with the effect of ice on the aerodynamic efficiency of a propeller, as compared to the efficiency loss associated with a heated-air anti-icing system. The propeller aerodynamic characteristics, thrust coefficient, and efficiency with and without the simulated ice are presented. A heated-air thermal anti-icing system for propellers is discussed and the results of an analysis of the losses inherent in such a system for an idealized case is presented. Two wind-tunnel investigations of propellers incorporating internal-flow systems are described: for one investigation the system was simplified almost to the ideal case, in the other investigation a propeller with a complete heated-air anti-icing system was used. The measured losses of efficiency are shown to be in good agreement with those predicted by theory
Notes:
Vendor supplied data
Publisher Number:
480037
Access Restriction:
Restricted for use by site license

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